2/137 failed unit tests - Mac OSX 10.11

[rich-cron]

Start testing: Feb 20 00:10 CET
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1/137 Testing: test_AerodynamicMomentAndAerodynamicForce
1/137 Test: test_AerodynamicMomentAndAerodynamicForce
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicMomentAndAerodynamicForce"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_AerodynamicMomentAndAerodynamicForce" start time: Feb 20 00:10 CET
Output:
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Running 3 test cases...
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type aerodynamic , acting on Vehicle, exerted by Earth
3, Rotation matrix from inertial frame to aerodynamic frame of Vehicle
12, Rotation matrix from inertial frame to body frame of Vehicle
21, Rotation matrix from inertial frame to corotating frame of Vehicle
30, Rotation matrix from inertial frame to trajectory frame of Vehicle
39, Airspeed-based velocity of Vehicle
42, Single acceleration in inertial frame of type thrust , acting on Vehicle

*** No errors detected
<end of output>
Test time =   3.94 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicMomentAndAerodynamicForce" end time: Feb 20 00:10 CET
"test_AerodynamicMomentAndAerodynamicForce" time elapsed: 00:00:03
----------------------------------------------------------

2/137 Testing: test_AerodynamicsNamespace
2/137 Test: test_AerodynamicsNamespace
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicsNamespace"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_AerodynamicsNamespace" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicsNamespace" end time: Feb 20 00:10 CET
"test_AerodynamicsNamespace" time elapsed: 00:00:00
----------------------------------------------------------

3/137 Testing: test_AerodynamicCoefficientGenerator
3/137 Test: test_AerodynamicCoefficientGenerator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicCoefficientGenerator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_AerodynamicCoefficientGenerator" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.04 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicCoefficientGenerator" end time: Feb 20 00:10 CET
"test_AerodynamicCoefficientGenerator" time elapsed: 00:00:00
----------------------------------------------------------

4/137 Testing: test_ExponentialAtmosphere
4/137 Test: test_ExponentialAtmosphere
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ExponentialAtmosphere"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_ExponentialAtmosphere" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ExponentialAtmosphere" end time: Feb 20 00:10 CET
"test_ExponentialAtmosphere" time elapsed: 00:00:00
----------------------------------------------------------

5/137 Testing: test_TabulatedAtmosphere
5/137 Test: test_TabulatedAtmosphere
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TabulatedAtmosphere"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_TabulatedAtmosphere" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.09 sec
----------------------------------------------------------
Test Passed.
"test_TabulatedAtmosphere" end time: Feb 20 00:10 CET
"test_TabulatedAtmosphere" time elapsed: 00:00:00
----------------------------------------------------------

6/137 Testing: test_TabulatedAerodynamicCoefficients
6/137 Test: test_TabulatedAerodynamicCoefficients
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TabulatedAerodynamicCoefficients"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_TabulatedAerodynamicCoefficients" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   1.90 sec
----------------------------------------------------------
Test Passed.
"test_TabulatedAerodynamicCoefficients" end time: Feb 20 00:10 CET
"test_TabulatedAerodynamicCoefficients" time elapsed: 00:00:01
----------------------------------------------------------

7/137 Testing: test_HeatTransfer
7/137 Test: test_HeatTransfer
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_HeatTransfer"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_HeatTransfer" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.02 sec
----------------------------------------------------------
Test Passed.
"test_HeatTransfer" end time: Feb 20 00:10 CET
"test_HeatTransfer" time elapsed: 00:00:00
----------------------------------------------------------

8/137 Testing: test_ControlSurfaceIncrements
8/137 Test: test_ControlSurfaceIncrements
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ControlSurfaceIncrements"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_ControlSurfaceIncrements" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Body orientation angle angle of attack of Apollo
2, Body orientation angle sideslip angle of Apollo
3, Control Surface Deflectionof Apollo w.r.t. TestSurface
4, Aerodynamic moment coefficients of Apollo
7, Aerodynamic force coefficients of Apollo

*** No errors detected
<end of output>
Test time =   0.36 sec
----------------------------------------------------------
Test Passed.
"test_ControlSurfaceIncrements" end time: Feb 20 00:10 CET
"test_ControlSurfaceIncrements" time elapsed: 00:00:00
----------------------------------------------------------

9/137 Testing: test_AerodynamicCoefficientsFromFile
9/137 Test: test_AerodynamicCoefficientsFromFile
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicCoefficientsFromFile"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_AerodynamicCoefficientsFromFile" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of SpacePlane
1, Body orientation angle angle of attack of SpacePlane
2, Body orientation angle sideslip angle of SpacePlane
3, Body orientation angle bank angle of SpacePlane
4, Aerodynamic moment coefficients of SpacePlane
7, Aerodynamic force coefficients of SpacePlane
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of SpacePlane
1, Body orientation angle angle of attack of SpacePlane
2, Body orientation angle sideslip angle of SpacePlane
3, Body orientation angle bank angle of SpacePlane
4, Control Surface Deflectionof SpacePlane w.r.t. TestSurface
5, Aerodynamic moment coefficients of SpacePlane
8, Aerodynamic force coefficients of SpacePlane
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of SpacePlane
1, Body orientation angle angle of attack of SpacePlane
2, Body orientation angle sideslip angle of SpacePlane
3, Body orientation angle bank angle of SpacePlane
4, Control Surface Deflectionof SpacePlane w.r.t. TestSurface
5, Aerodynamic moment coefficients of SpacePlane
8, Aerodynamic force coefficients of SpacePlane

*** No errors detected
<end of output>
Test time =   0.25 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicCoefficientsFromFile" end time: Feb 20 00:10 CET
"test_AerodynamicCoefficientsFromFile" time elapsed: 00:00:00
----------------------------------------------------------

10/137 Testing: test_NRLMSISE00Atmosphere
10/137 Test: test_NRLMSISE00Atmosphere
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_NRLMSISE00Atmosphere"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Aerodynamics
"test_NRLMSISE00Atmosphere" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 24 test cases...

*** No errors detected
<end of output>
Test time =   0.03 sec
----------------------------------------------------------
Test Passed.
"test_NRLMSISE00Atmosphere" end time: Feb 20 00:10 CET
"test_NRLMSISE00Atmosphere" time elapsed: 00:00:00
----------------------------------------------------------

11/137 Testing: test_AstrodynamicsFunctions
11/137 Test: test_AstrodynamicsFunctions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AstrodynamicsFunctions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_AstrodynamicsFunctions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_AstrodynamicsFunctions" end time: Feb 20 00:10 CET
"test_AstrodynamicsFunctions" time elapsed: 00:00:00
----------------------------------------------------------

12/137 Testing: test_OrbitalElementConversions
12/137 Test: test_OrbitalElementConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_OrbitalElementConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_OrbitalElementConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 11 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_OrbitalElementConversions" end time: Feb 20 00:10 CET
"test_OrbitalElementConversions" time elapsed: 00:00:00
----------------------------------------------------------

13/137 Testing: test_PhysicalConstants
13/137 Test: test_PhysicalConstants
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_PhysicalConstants"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_PhysicalConstants" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_PhysicalConstants" end time: Feb 20 00:10 CET
"test_PhysicalConstants" time elapsed: 00:00:00
----------------------------------------------------------

14/137 Testing: test_UnitConversions
14/137 Test: test_UnitConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_UnitConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_UnitConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 14 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_UnitConversions" end time: Feb 20 00:10 CET
"test_UnitConversions" time elapsed: 00:00:00
----------------------------------------------------------

15/137 Testing: test_MeanToEccentricAnomalyConversion
15/137 Test: test_MeanToEccentricAnomalyConversion
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MeanToEccentricAnomalyConversion"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_MeanToEccentricAnomalyConversion" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 7 test cases...

*** No errors detected
<end of output>
Test time =   1.00 sec
----------------------------------------------------------
Test Passed.
"test_MeanToEccentricAnomalyConversion" end time: Feb 20 00:10 CET
"test_MeanToEccentricAnomalyConversion" time elapsed: 00:00:00
----------------------------------------------------------

16/137 Testing: test_MeanToHyperbolicEccentricAnomalyConversion
16/137 Test: test_MeanToHyperbolicEccentricAnomalyConversion
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MeanToHyperbolicEccentricAnomalyConversion"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_MeanToHyperbolicEccentricAnomalyConversion" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   1.59 sec
----------------------------------------------------------
Test Passed.
"test_MeanToHyperbolicEccentricAnomalyConversion" end time: Feb 20 00:10 CET
"test_MeanToHyperbolicEccentricAnomalyConversion" time elapsed: 00:00:01
----------------------------------------------------------

17/137 Testing: test_KeplerPropagator
17/137 Test: test_KeplerPropagator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_KeplerPropagator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_KeplerPropagator" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 6 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_KeplerPropagator" end time: Feb 20 00:10 CET
"test_KeplerPropagator" time elapsed: 00:00:00
----------------------------------------------------------

18/137 Testing: test_AccelerationModel
18/137 Test: test_AccelerationModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AccelerationModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_AccelerationModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_AccelerationModel" end time: Feb 20 00:10 CET
"test_AccelerationModel" time elapsed: 00:00:00
----------------------------------------------------------

19/137 Testing: test_ClohessyWiltshirePropagator
19/137 Test: test_ClohessyWiltshirePropagator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ClohessyWiltshirePropagator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_ClohessyWiltshirePropagator" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ClohessyWiltshirePropagator" end time: Feb 20 00:10 CET
"test_ClohessyWiltshirePropagator" time elapsed: 00:00:00
----------------------------------------------------------

20/137 Testing: test_MissionGeometry
20/137 Test: test_MissionGeometry
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MissionGeometry"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_MissionGeometry" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 6 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_MissionGeometry" end time: Feb 20 00:10 CET
"test_MissionGeometry" time elapsed: 00:00:00
----------------------------------------------------------

21/137 Testing: test_TimeConversions
21/137 Test: test_TimeConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TimeConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_TimeConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_TimeConversions" end time: Feb 20 00:10 CET
"test_TimeConversions" time elapsed: 00:00:00
----------------------------------------------------------

22/137 Testing: test_CelestialBodyConstants
22/137 Test: test_CelestialBodyConstants
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CelestialBodyConstants"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_CelestialBodyConstants" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_CelestialBodyConstants" end time: Feb 20 00:10 CET
"test_CelestialBodyConstants" time elapsed: 00:00:00
----------------------------------------------------------

23/137 Testing: test_ModifiedEquinoctialElementConversions
23/137 Test: test_ModifiedEquinoctialElementConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ModifiedEquinoctialElementConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_ModifiedEquinoctialElementConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ModifiedEquinoctialElementConversions" end time: Feb 20 00:10 CET
"test_ModifiedEquinoctialElementConversions" time elapsed: 00:00:00
----------------------------------------------------------

24/137 Testing: test_GeodeticCoordinateConversions
24/137 Test: test_GeodeticCoordinateConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_GeodeticCoordinateConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_GeodeticCoordinateConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_GeodeticCoordinateConversions" end time: Feb 20 00:10 CET
"test_GeodeticCoordinateConversions" time elapsed: 00:00:00
----------------------------------------------------------

25/137 Testing: test_StateElementConversions
25/137 Test: test_StateElementConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_StateElementConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_StateElementConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_StateElementConversions" end time: Feb 20 00:10 CET
"test_StateElementConversions" time elapsed: 00:00:00
----------------------------------------------------------

26/137 Testing: test_SphericalOrbitalStateConversions
26/137 Test: test_SphericalOrbitalStateConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SphericalOrbitalStateConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_SphericalOrbitalStateConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_SphericalOrbitalStateConversions" end time: Feb 20 00:10 CET
"test_SphericalOrbitalStateConversions" time elapsed: 00:00:00
----------------------------------------------------------

27/137 Testing: test_BodyShapeModels
27/137 Test: test_BodyShapeModels
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_BodyShapeModels"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_BodyShapeModels" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_BodyShapeModels" end time: Feb 20 00:10 CET
"test_BodyShapeModels" time elapsed: 00:00:00
----------------------------------------------------------

28/137 Testing: test_UnifiedStateModelElementConversions
28/137 Test: test_UnifiedStateModelElementConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_UnifiedStateModelElementConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/BasicAstrodynamics
"test_UnifiedStateModelElementConversions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_UnifiedStateModelElementConversions" end time: Feb 20 00:10 CET
"test_UnifiedStateModelElementConversions" time elapsed: 00:00:00
----------------------------------------------------------

29/137 Testing: test_CannonBallRadiationPressureAccelerationAndForce
29/137 Test: test_CannonBallRadiationPressureAccelerationAndForce
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CannonBallRadiationPressureAccelerationAndForce"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism
"test_CannonBallRadiationPressureAccelerationAndForce" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 9 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_CannonBallRadiationPressureAccelerationAndForce" end time: Feb 20 00:10 CET
"test_CannonBallRadiationPressureAccelerationAndForce" time elapsed: 00:00:00
----------------------------------------------------------

30/137 Testing: test_LorentzStaticMagneticAccelerationAndForce
30/137 Test: test_LorentzStaticMagneticAccelerationAndForce
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LorentzStaticMagneticAccelerationAndForce"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism
"test_LorentzStaticMagneticAccelerationAndForce" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LorentzStaticMagneticAccelerationAndForce" end time: Feb 20 00:10 CET
"test_LorentzStaticMagneticAccelerationAndForce" time elapsed: 00:00:00
----------------------------------------------------------

31/137 Testing: test_RadiationPressureInterface
31/137 Test: test_RadiationPressureInterface
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RadiationPressureInterface"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ElectroMagnetism
"test_RadiationPressureInterface" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_RadiationPressureInterface" end time: Feb 20 00:10 CET
"test_RadiationPressureInterface" time elapsed: 00:00:00
----------------------------------------------------------

32/137 Testing: test_ApproximatePlanetPositions
32/137 Test: test_ApproximatePlanetPositions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ApproximatePlanetPositions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_ApproximatePlanetPositions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ApproximatePlanetPositions" end time: Feb 20 00:10 CET
"test_ApproximatePlanetPositions" time elapsed: 00:00:00
----------------------------------------------------------

33/137 Testing: test_TabulatedEphemeris
33/137 Test: test_TabulatedEphemeris
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TabulatedEphemeris"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_TabulatedEphemeris" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.06 sec
----------------------------------------------------------
Test Passed.
"test_TabulatedEphemeris" end time: Feb 20 00:10 CET
"test_TabulatedEphemeris" time elapsed: 00:00:00
----------------------------------------------------------

34/137 Testing: test_CartesianStateExtractor
34/137 Test: test_CartesianStateExtractor
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CartesianStateExtractor"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_CartesianStateExtractor" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 7 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_CartesianStateExtractor" end time: Feb 20 00:10 CET
"test_CartesianStateExtractor" time elapsed: 00:00:00
----------------------------------------------------------

35/137 Testing: test_KeplerStateExtractor
35/137 Test: test_KeplerStateExtractor
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_KeplerStateExtractor"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_KeplerStateExtractor" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 8 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_KeplerStateExtractor" end time: Feb 20 00:10 CET
"test_KeplerStateExtractor" time elapsed: 00:00:00
----------------------------------------------------------

36/137 Testing: test_RotationalEphemeris
36/137 Test: test_RotationalEphemeris
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RotationalEphemeris"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_RotationalEphemeris" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_RotationalEphemeris" end time: Feb 20 00:10 CET
"test_RotationalEphemeris" time elapsed: 00:00:00
----------------------------------------------------------

37/137 Testing: test_SimpleRotationalEphemeris
37/137 Test: test_SimpleRotationalEphemeris
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SimpleRotationalEphemeris"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_SimpleRotationalEphemeris" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_SimpleRotationalEphemeris" end time: Feb 20 00:10 CET
"test_SimpleRotationalEphemeris" time elapsed: 00:00:00
----------------------------------------------------------

38/137 Testing: test_FrameManager
38/137 Test: test_FrameManager
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_FrameManager"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_FrameManager" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.08 sec
----------------------------------------------------------
Test Passed.
"test_FrameManager" end time: Feb 20 00:10 CET
"test_FrameManager" time elapsed: 00:00:00
----------------------------------------------------------

39/137 Testing: test_CompositeEphemeris
39/137 Test: test_CompositeEphemeris
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CompositeEphemeris"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_CompositeEphemeris" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.14 sec
----------------------------------------------------------
Test Passed.
"test_CompositeEphemeris" end time: Feb 20 00:10 CET
"test_CompositeEphemeris" time elapsed: 00:00:00
----------------------------------------------------------

40/137 Testing: test_KeplerEphemeris
40/137 Test: test_KeplerEphemeris
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_KeplerEphemeris"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Ephemerides
"test_KeplerEphemeris" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_KeplerEphemeris" end time: Feb 20 00:10 CET
"test_KeplerEphemeris" time elapsed: 00:00:00
----------------------------------------------------------

41/137 Testing: test_SphericalHarmonicsGravityField
41/137 Test: test_SphericalHarmonicsGravityField
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SphericalHarmonicsGravityField"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_SphericalHarmonicsGravityField" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_SphericalHarmonicsGravityField" end time: Feb 20 00:10 CET
"test_SphericalHarmonicsGravityField" time elapsed: 00:00:00
----------------------------------------------------------

42/137 Testing: test_GravitationalForce
42/137 Test: test_GravitationalForce
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_GravitationalForce"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_GravitationalForce" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_GravitationalForce" end time: Feb 20 00:10 CET
"test_GravitationalForce" time elapsed: 00:00:00
----------------------------------------------------------

43/137 Testing: test_CentralAndZonalGravityModel
43/137 Test: test_CentralAndZonalGravityModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CentralAndZonalGravityModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_CentralAndZonalGravityModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.02 sec
----------------------------------------------------------
Test Passed.
"test_CentralAndZonalGravityModel" end time: Feb 20 00:10 CET
"test_CentralAndZonalGravityModel" time elapsed: 00:00:00
----------------------------------------------------------

44/137 Testing: test_UnitConversionsCircularRestrictedThreeBodyProblem
44/137 Test: test_UnitConversionsCircularRestrictedThreeBodyProblem
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_UnitConversionsCircularRestrictedThreeBodyProblem"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_UnitConversionsCircularRestrictedThreeBodyProblem" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_UnitConversionsCircularRestrictedThreeBodyProblem" end time: Feb 20 00:10 CET
"test_UnitConversionsCircularRestrictedThreeBodyProblem" time elapsed: 00:00:00
----------------------------------------------------------

45/137 Testing: test_JacobiEnergy
45/137 Test: test_JacobiEnergy
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_JacobiEnergy"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_JacobiEnergy" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_JacobiEnergy" end time: Feb 20 00:10 CET
"test_JacobiEnergy" time elapsed: 00:00:00
----------------------------------------------------------

46/137 Testing: test_LibrationPoints
46/137 Test: test_LibrationPoints
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LibrationPoints"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_LibrationPoints" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 6 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LibrationPoints" end time: Feb 20 00:10 CET
"test_LibrationPoints" time elapsed: 00:00:00
----------------------------------------------------------

47/137 Testing: test_StateDerivativeRestrictedThreeBodyProblem
47/137 Test: test_StateDerivativeRestrictedThreeBodyProblem
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_StateDerivativeRestrictedThreeBodyProblem"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_StateDerivativeRestrictedThreeBodyProblem" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_StateDerivativeRestrictedThreeBodyProblem" end time: Feb 20 00:10 CET
"test_StateDerivativeRestrictedThreeBodyProblem" time elapsed: 00:00:00
----------------------------------------------------------

48/137 Testing: test_SphericalHarmonicsGravityModel
48/137 Test: test_SphericalHarmonicsGravityModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SphericalHarmonicsGravityModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_SphericalHarmonicsGravityModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_SphericalHarmonicsGravityModel" end time: Feb 20 00:10 CET
"test_SphericalHarmonicsGravityModel" time elapsed: 00:00:00
----------------------------------------------------------

49/137 Testing: test_ThirdBodyPerturbation
49/137 Test: test_ThirdBodyPerturbation
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ThirdBodyPerturbation"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_ThirdBodyPerturbation" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ThirdBodyPerturbation" end time: Feb 20 00:10 CET
"test_ThirdBodyPerturbation" time elapsed: 00:00:00
----------------------------------------------------------

50/137 Testing: test_TriAxialEllipsoidGravity
50/137 Test: test_TriAxialEllipsoidGravity
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TriAxialEllipsoidGravity"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_TriAxialEllipsoidGravity" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_TriAxialEllipsoidGravity" end time: Feb 20 00:10 CET
"test_TriAxialEllipsoidGravity" time elapsed: 00:00:00
----------------------------------------------------------

51/137 Testing: test_GravityFieldVariations
51/137 Test: test_GravityFieldVariations
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_GravityFieldVariations"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_GravityFieldVariations" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.09 sec
----------------------------------------------------------
Test Passed.
"test_GravityFieldVariations" end time: Feb 20 00:10 CET
"test_GravityFieldVariations" time elapsed: 00:00:00
----------------------------------------------------------

52/137 Testing: test_MutualSphericalHarmonicsGravityModel
52/137 Test: test_MutualSphericalHarmonicsGravityModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MutualSphericalHarmonicsGravityModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Gravitation
"test_MutualSphericalHarmonicsGravityModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.11 sec
----------------------------------------------------------
Test Passed.
"test_MutualSphericalHarmonicsGravityModel" end time: Feb 20 00:10 CET
"test_MutualSphericalHarmonicsGravityModel" time elapsed: 00:00:00
----------------------------------------------------------

53/137 Testing: test_EscapeAndCapture
53/137 Test: test_EscapeAndCapture
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_EscapeAndCapture"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_EscapeAndCapture" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_EscapeAndCapture" end time: Feb 20 00:10 CET
"test_EscapeAndCapture" time elapsed: 00:00:00
----------------------------------------------------------

54/137 Testing: test_GravityAssist
54/137 Test: test_GravityAssist
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_GravityAssist"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_GravityAssist" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 14 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_GravityAssist" end time: Feb 20 00:10 CET
"test_GravityAssist" time elapsed: 00:00:00
----------------------------------------------------------

55/137 Testing: test_LambertTargeterIzzo
55/137 Test: test_LambertTargeterIzzo
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LambertTargeterIzzo"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_LambertTargeterIzzo" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LambertTargeterIzzo" end time: Feb 20 00:10 CET
"test_LambertTargeterIzzo" time elapsed: 00:00:00
----------------------------------------------------------

56/137 Testing: test_LambertTargeterGooding
56/137 Test: test_LambertTargeterGooding
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LambertTargeterGooding"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_LambertTargeterGooding" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LambertTargeterGooding" end time: Feb 20 00:10 CET
"test_LambertTargeterGooding" time elapsed: 00:00:00
----------------------------------------------------------

57/137 Testing: test_LambertTargeter
57/137 Test: test_LambertTargeter
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LambertTargeter"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_LambertTargeter" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LambertTargeter" end time: Feb 20 00:10 CET
"test_LambertTargeter" time elapsed: 00:00:00
----------------------------------------------------------

58/137 Testing: test_LambertRoutines
58/137 Test: test_LambertRoutines
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LambertRoutines"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_LambertRoutines" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 13 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LambertRoutines" end time: Feb 20 00:10 CET
"test_LambertRoutines" time elapsed: 00:00:00
----------------------------------------------------------

59/137 Testing: test_ZeroRevolutionLambertTargeterIzzo
59/137 Test: test_ZeroRevolutionLambertTargeterIzzo
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ZeroRevolutionLambertTargeterIzzo"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_ZeroRevolutionLambertTargeterIzzo" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ZeroRevolutionLambertTargeterIzzo" end time: Feb 20 00:10 CET
"test_ZeroRevolutionLambertTargeterIzzo" time elapsed: 00:00:00
----------------------------------------------------------

60/137 Testing: test_MultiRevolutionLambertTargeterIzzo
60/137 Test: test_MultiRevolutionLambertTargeterIzzo
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MultiRevolutionLambertTargeterIzzo"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_MultiRevolutionLambertTargeterIzzo" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_MultiRevolutionLambertTargeterIzzo" end time: Feb 20 00:10 CET
"test_MultiRevolutionLambertTargeterIzzo" time elapsed: 00:00:00
----------------------------------------------------------

61/137 Testing: test_MathematicalShapeFunctions
61/137 Test: test_MathematicalShapeFunctions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MathematicalShapeFunctions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/MissionSegments
"test_MathematicalShapeFunctions" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_MathematicalShapeFunctions" end time: Feb 20 00:10 CET
"test_MathematicalShapeFunctions" time elapsed: 00:00:00
----------------------------------------------------------

62/137 Testing: test_ReferenceFrameTransformations
62/137 Test: test_ReferenceFrameTransformations
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ReferenceFrameTransformations"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames
"test_ReferenceFrameTransformations" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 10 test cases...

*** No errors detected
<end of output>
Test time =   0.03 sec
----------------------------------------------------------
Test Passed.
"test_ReferenceFrameTransformations" end time: Feb 20 00:10 CET
"test_ReferenceFrameTransformations" time elapsed: 00:00:00
----------------------------------------------------------

63/137 Testing: test_ApparentAccelerationModel
63/137 Test: test_ApparentAccelerationModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ApparentAccelerationModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames
"test_ApparentAccelerationModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ApparentAccelerationModel" end time: Feb 20 00:10 CET
"test_ApparentAccelerationModel" time elapsed: 00:00:00
----------------------------------------------------------

64/137 Testing: test_AerodynamicAngleCalculator
64/137 Test: test_AerodynamicAngleCalculator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicAngleCalculator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ReferenceFrames
"test_AerodynamicAngleCalculator" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicAngleCalculator" end time: Feb 20 00:10 CET
"test_AerodynamicAngleCalculator" time elapsed: 00:00:00
----------------------------------------------------------

65/137 Testing: test_LightTime
65/137 Test: test_LightTime
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LightTime"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels
"test_LightTime" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.08 sec
----------------------------------------------------------
Test Passed.
"test_LightTime" end time: Feb 20 00:10 CET
"test_LightTime" time elapsed: 00:00:00
----------------------------------------------------------

66/137 Testing: test_AngularPositionModel
66/137 Test: test_AngularPositionModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AngularPositionModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels
"test_AngularPositionModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...
Warning, position of Mars taken as barycenter of that body's planetary system.

*** No errors detected
<end of output>
Test time =   0.13 sec
----------------------------------------------------------
Test Passed.
"test_AngularPositionModel" end time: Feb 20 00:10 CET
"test_AngularPositionModel" time elapsed: 00:00:00
----------------------------------------------------------

67/137 Testing: test_OneWayRangeModel
67/137 Test: test_OneWayRangeModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_OneWayRangeModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels
"test_OneWayRangeModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...
Warning, position of Mars taken as barycenter of that body's planetary system.

*** No errors detected
<end of output>
Test time =   0.12 sec
----------------------------------------------------------
Test Passed.
"test_OneWayRangeModel" end time: Feb 20 00:10 CET
"test_OneWayRangeModel" time elapsed: 00:00:00
----------------------------------------------------------

68/137 Testing: test_PositionObservationModel
68/137 Test: test_PositionObservationModel
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_PositionObservationModel"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/ObservationModels
"test_PositionObservationModel" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.12 sec
----------------------------------------------------------
Test Passed.
"test_PositionObservationModel" end time: Feb 20 00:10 CET
"test_PositionObservationModel" time elapsed: 00:00:00
----------------------------------------------------------

69/137 Testing: test_AccelerationPartials
69/137 Test: test_AccelerationPartials
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AccelerationPartials"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/AccelerationPartials
"test_AccelerationPartials" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.05 sec
----------------------------------------------------------
Test Passed.
"test_AccelerationPartials" end time: Feb 20 00:10 CET
"test_AccelerationPartials" time elapsed: 00:00:00
----------------------------------------------------------

70/137 Testing: test_SphericalHarmonicPartials
70/137 Test: test_SphericalHarmonicPartials
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SphericalHarmonicPartials"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/AccelerationPartials
"test_SphericalHarmonicPartials" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.09 sec
----------------------------------------------------------
Test Passed.
"test_SphericalHarmonicPartials" end time: Feb 20 00:10 CET
"test_SphericalHarmonicPartials" time elapsed: 00:00:00
----------------------------------------------------------

71/137 Testing: test_RotationMatrixPartials
71/137 Test: test_RotationMatrixPartials
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RotationMatrixPartials"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/OrbitDetermination/ObservationPartials
"test_RotationMatrixPartials" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.08 sec
----------------------------------------------------------
Test Passed.
"test_RotationMatrixPartials" end time: Feb 20 00:10 CET
"test_RotationMatrixPartials" time elapsed: 00:00:00
----------------------------------------------------------

72/137 Testing: test_CentralBodyData
72/137 Test: test_CentralBodyData
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CentralBodyData"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_CentralBodyData" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_CentralBodyData" end time: Feb 20 00:10 CET
"test_CentralBodyData" time elapsed: 00:00:00
----------------------------------------------------------

73/137 Testing: test_CowellStateDerivative
73/137 Test: test_CowellStateDerivative
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CowellStateDerivative"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_CowellStateDerivative" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 2 test cases...
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
unknown location:0: fatal error in "testCowellPopagatorKeplerCompare": signal: SIGSEGV, si_code: 0 (memory access violation at address: 0x00000000)
/Users/richardcronheim/tudatBundle-rich-cron/tudat/Tudat/Astrodynamics/Propagators/UnitTests/unitTestCowellStateDerivative.cpp:479: last checkpoint

*** 1 failure detected in test suite "Master Test Suite"
<end of output>
Test time =   9.42 sec
----------------------------------------------------------
Test Failed.
"test_CowellStateDerivative" end time: Feb 20 00:10 CET
"test_CowellStateDerivative" time elapsed: 00:00:09
----------------------------------------------------------

74/137 Testing: test_EnckeStateDerivative
74/137 Test: test_EnckeStateDerivative
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_EnckeStateDerivative"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_EnckeStateDerivative" start time: Feb 20 00:10 CET
Output:
----------------------------------------------------------
Running 3 test cases...
Warning, position of Jupiter taken as barycenter of that body's planetary system.
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Jupiter taken as barycenter of that body's planetary system.
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Testint with eccentricity 0.8Testint with eccentricity 0.9Testint with eccentricity 0.95Testint with eccentricity 0.99
*** No errors detected
<end of output>
Test time =  11.22 sec
----------------------------------------------------------
Test Passed.
"test_EnckeStateDerivative" end time: Feb 20 00:11 CET
"test_EnckeStateDerivative" time elapsed: 00:00:11
----------------------------------------------------------

75/137 Testing: test_SequentialVariationEquationIntegration
75/137 Test: test_SequentialVariationEquationIntegration
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SequentialVariationEquationIntegration"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_SequentialVariationEquationIntegration" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision

*** No errors detected
<end of output>
Test time =   6.31 sec
----------------------------------------------------------
Test Passed.
"test_SequentialVariationEquationIntegration" end time: Feb 20 00:11 CET
"test_SequentialVariationEquationIntegration" time elapsed: 00:00:06
----------------------------------------------------------

76/137 Testing: test_VariationalEquations
76/137 Test: test_VariationalEquations
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_VariationalEquations"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_VariationalEquations" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, position of Mars taken as barycenter of that body's planetary system.
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision

*** No errors detected
<end of output>
Test time =  24.37 sec
----------------------------------------------------------
Test Passed.
"test_VariationalEquations" end time: Feb 20 00:11 CET
"test_VariationalEquations" time elapsed: 00:00:24
----------------------------------------------------------

77/137 Testing: test_EnvironmentModelUpdater
77/137 Test: test_EnvironmentModelUpdater
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_EnvironmentModelUpdater"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_EnvironmentModelUpdater" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...
Warning, position of Mars taken as barycenter of that body's planetary system.

*** No errors detected
<end of output>
Test time =   0.27 sec
----------------------------------------------------------
Test Passed.
"test_EnvironmentModelUpdater" end time: Feb 20 00:11 CET
"test_EnvironmentModelUpdater" time elapsed: 00:00:00
----------------------------------------------------------

78/137 Testing: test_BodyMassPropagation
78/137 Test: test_BodyMassPropagation
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_BodyMassPropagation"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_BodyMassPropagation" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.04 sec
----------------------------------------------------------
Test Passed.
"test_BodyMassPropagation" end time: Feb 20 00:11 CET
"test_BodyMassPropagation" time elapsed: 00:00:00
----------------------------------------------------------

79/137 Testing: test_MultiTypeStatePropagation
79/137 Test: test_MultiTypeStatePropagation
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MultiTypeStatePropagation"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_MultiTypeStatePropagation" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision
Warning, tabulated ephemeris is being reset using data at different precision

*** No errors detected
<end of output>
Test time =   0.64 sec
----------------------------------------------------------
Test Passed.
"test_MultiTypeStatePropagation" end time: Feb 20 00:11 CET
"test_MultiTypeStatePropagation" time elapsed: 00:00:00
----------------------------------------------------------

80/137 Testing: test_DependentVariableOutput
80/137 Test: test_DependentVariableOutput
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_DependentVariableOutput"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_DependentVariableOutput" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Altitude of Apollo w.r.t. Earth
2, Relative distance of Apollo w.r.t. Earth
3, Relative speed of Apollo w.r.t. Earth
4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth
5, Aerodynamic g-load of Apollo w.r.t. Earth
6, Stagnation-point heat flux of Apollo w.r.t. Earth
7, Local freestream temperature of Apollo w.r.t. Earth
8, Geodetic latitude of Apollo w.r.t. Earth
9, Density of Apollo w.r.t. Earth
10, Body orientation angle latitude angle of Apollo
11, Body orientation angle longitude angle of Apollo
12, Body orientation angle angle of attack of Apollo
13, Body orientation angle sideslip angle of Apollo
14, Body orientation angle bank angle of Apollo
15, Relative position of Apollo w.r.t. Earth
18, Relative velocity of Apollo w.r.t. Earth
21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth
24, Total acceleration in inertial frame of Apollo
27, Aerodynamic moment coefficients of Apollo
30, Aerodynamic force coefficients of Apollo
33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
Propagated
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Altitude of Apollo w.r.t. Earth
2, Relative distance of Apollo w.r.t. Earth
3, Relative speed of Apollo w.r.t. Earth
4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth
5, Aerodynamic g-load of Apollo w.r.t. Earth
6, Stagnation-point heat flux of Apollo w.r.t. Earth
7, Local freestream temperature of Apollo w.r.t. Earth
8, Geodetic latitude of Apollo w.r.t. Earth
9, Density of Apollo w.r.t. Earth
10, Body orientation angle latitude angle of Apollo
11, Body orientation angle longitude angle of Apollo
12, Body orientation angle angle of attack of Apollo
13, Body orientation angle sideslip angle of Apollo
14, Body orientation angle bank angle of Apollo
15, Relative position of Apollo w.r.t. Earth
18, Relative velocity of Apollo w.r.t. Earth
21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth
24, Total acceleration in inertial frame of Apollo
27, Aerodynamic moment coefficients of Apollo
30, Aerodynamic force coefficients of Apollo
33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
Propagated
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Altitude of Apollo w.r.t. Earth
2, Relative distance of Apollo w.r.t. Earth
3, Relative speed of Apollo w.r.t. Earth
4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth
5, Aerodynamic g-load of Apollo w.r.t. Earth
6, Stagnation-point heat flux of Apollo w.r.t. Earth
7, Local freestream temperature of Apollo w.r.t. Earth
8, Geodetic latitude of Apollo w.r.t. Earth
9, Density of Apollo w.r.t. Earth
10, Body orientation angle latitude angle of Apollo
11, Body orientation angle longitude angle of Apollo
12, Body orientation angle angle of attack of Apollo
13, Body orientation angle sideslip angle of Apollo
14, Body orientation angle bank angle of Apollo
15, Relative position of Apollo w.r.t. Earth
18, Relative velocity of Apollo w.r.t. Earth
21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth
24, Total acceleration in inertial frame of Apollo
27, Aerodynamic moment coefficients of Apollo
30, Aerodynamic force coefficients of Apollo
33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
Propagated
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Altitude of Apollo w.r.t. Earth
2, Relative distance of Apollo w.r.t. Earth
3, Relative speed of Apollo w.r.t. Earth
4, Single acceleration norm of type central gravity , acting on Apollo, exerted by Earth
5, Aerodynamic g-load of Apollo w.r.t. Earth
6, Stagnation-point heat flux of Apollo w.r.t. Earth
7, Local freestream temperature of Apollo w.r.t. Earth
8, Geodetic latitude of Apollo w.r.t. Earth
9, Density of Apollo w.r.t. Earth
10, Body orientation angle latitude angle of Apollo
11, Body orientation angle longitude angle of Apollo
12, Body orientation angle angle of attack of Apollo
13, Body orientation angle sideslip angle of Apollo
14, Body orientation angle bank angle of Apollo
15, Relative position of Apollo w.r.t. Earth
18, Relative velocity of Apollo w.r.t. Earth
21, Single acceleration in inertial frame of type central gravity , acting on Apollo, exerted by Earth
24, Total acceleration in inertial frame of Apollo
27, Aerodynamic moment coefficients of Apollo
30, Aerodynamic force coefficients of Apollo
33, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
Propagated

*** No errors detected
<end of output>
Test time =   7.06 sec
----------------------------------------------------------
Test Passed.
"test_DependentVariableOutput" end time: Feb 20 00:11 CET
"test_DependentVariableOutput" time elapsed: 00:00:07
----------------------------------------------------------

81/137 Testing: test_StoppingConditions
81/137 Test: test_StoppingConditions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_StoppingConditions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_StoppingConditions" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   1.90 sec
----------------------------------------------------------
Test Passed.
"test_StoppingConditions" end time: Feb 20 00:11 CET
"test_StoppingConditions" time elapsed: 00:00:01
----------------------------------------------------------

82/137 Testing: test_CustomStatePropagation
82/137 Test: test_CustomStatePropagation
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CustomStatePropagation"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propagators
"test_CustomStatePropagation" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 5 test cases...
Warning, tabulated ephemeris is being reset using data at different precision

*** No errors detected
<end of output>
Test time =   0.29 sec
----------------------------------------------------------
Test Passed.
"test_CustomStatePropagation" end time: Feb 20 00:11 CET
"test_CustomStatePropagation" time elapsed: 00:00:00
----------------------------------------------------------

83/137 Testing: test_ShapiroTimeDelay
83/137 Test: test_ShapiroTimeDelay
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ShapiroTimeDelay"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Relativity
"test_ShapiroTimeDelay" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ShapiroTimeDelay" end time: Feb 20 00:11 CET
"test_ShapiroTimeDelay" time elapsed: 00:00:00
----------------------------------------------------------

84/137 Testing: test_ThrustAcceleration
84/137 Test: test_ThrustAcceleration
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ThrustAcceleration"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/Propulsion
"test_ThrustAcceleration" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 8 test cases...
Warning, cannot reset dependentOrientationCalculator, incompatible object already exists
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type thrust , acting on Vehicle
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Body orientation angle angle of attack of Apollo
2, Body orientation angle sideslip angle of Apollo
3, Body orientation angle bank angle of Apollo
4, Airspeed of Apollo w.r.t. Earth
5, Density of Apollo w.r.t. Earth
6, Rotation matrix from inertial frame to body frame of Apollo
15, Rotation matrix to body-fixed frame of Apollo
24, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
27, Single acceleration in inertial frame of type thrust , acting on Apollo
30, Aerodynamic force coefficients of Apollo
33, Aerodynamic moment coefficients of Apollo
36, Rotation matrix from inertial frame to aerodynamic frame of Apollo
45, Rotation matrix from aerodynamic frame to body frame of Apollo
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Body orientation angle angle of attack of Apollo
2, Body orientation angle sideslip angle of Apollo
3, Body orientation angle bank angle of Apollo
4, Airspeed of Apollo w.r.t. Earth
5, Density of Apollo w.r.t. Earth
6, Rotation matrix from inertial frame to body frame of Apollo
15, Rotation matrix to body-fixed frame of Apollo
24, Single acceleration in inertial frame of type aerodynamic , acting on Apollo, exerted by Earth
27, Single acceleration in inertial frame of type thrust , acting on Apollo
30, Aerodynamic force coefficients of Apollo
33, Aerodynamic moment coefficients of Apollo
36, Rotation matrix from inertial frame to aerodynamic frame of Apollo
45, Rotation matrix from aerodynamic frame to body frame of Apollo
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type thrust , acting on Asterix
3, Relative position of Asterix w.r.t. Earth
6, Relative velocity of Asterix w.r.t. Earth
9, LVLH to inertial frame rotation matrixof Asterix w.r.t. Earth
Warning, cannot reset dependentOrientationCalculator, incompatible object already exists
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration in inertial frame of type thrust , acting on Asterix
3, Relative position of Asterix w.r.t. Earth
6, Relative velocity of Asterix w.r.t. Earth
9, LVLH to inertial frame rotation matrixof Asterix w.r.t. Earth
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Mach number of Apollo
1, Airspeed of Apollo
2, Density of Apollo
3, Single acceleration norm of type thrust , acting on Apollo
4, Body mass rateof Apollo
Dependent variables being saved, output vectors contain: 
Vector entry, Vector contents
0, Single acceleration norm of type thrust , acting on Apollo

*** No errors detected
<end of output>
Test time =   4.47 sec
----------------------------------------------------------
Test Passed.
"test_ThrustAcceleration" end time: Feb 20 00:11 CET
"test_ThrustAcceleration" time elapsed: 00:00:04
----------------------------------------------------------

85/137 Testing: test_GroundStationState
85/137 Test: test_GroundStationState
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_GroundStationState"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Astrodynamics/GroundStations
"test_GroundStationState" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.06 sec
----------------------------------------------------------
Test Passed.
"test_GroundStationState" end time: Feb 20 00:11 CET
"test_GroundStationState" time elapsed: 00:00:00
----------------------------------------------------------

86/137 Testing: test_TimeTypes
86/137 Test: test_TimeTypes
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TimeTypes"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Basics
"test_TimeTypes" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_TimeTypes" end time: Feb 20 00:11 CET
"test_TimeTypes" time elapsed: 00:00:00
----------------------------------------------------------

87/137 Testing: test_MatrixTextFileReader
87/137 Test: test_MatrixTextFileReader
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MatrixTextFileReader"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_MatrixTextFileReader" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_MatrixTextFileReader" end time: Feb 20 00:11 CET
"test_MatrixTextFileReader" time elapsed: 00:00:00
----------------------------------------------------------

88/137 Testing: test_StreamFilters
88/137 Test: test_StreamFilters
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_StreamFilters"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_StreamFilters" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 8 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_StreamFilters" end time: Feb 20 00:11 CET
"test_StreamFilters" time elapsed: 00:00:00
----------------------------------------------------------

89/137 Testing: test_TwoLineElementsTextFileReader
89/137 Test: test_TwoLineElementsTextFileReader
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TwoLineElementsTextFileReader"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_TwoLineElementsTextFileReader" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_TwoLineElementsTextFileReader" end time: Feb 20 00:11 CET
"test_TwoLineElementsTextFileReader" time elapsed: 00:00:00
----------------------------------------------------------

90/137 Testing: test_BasicInputOutput
90/137 Test: test_BasicInputOutput
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_BasicInputOutput"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_BasicInputOutput" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_BasicInputOutput" end time: Feb 20 00:11 CET
"test_BasicInputOutput" time elapsed: 00:00:00
----------------------------------------------------------

91/137 Testing: test_ParsedDataVectorUtilities
91/137 Test: test_ParsedDataVectorUtilities
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_ParsedDataVectorUtilities"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_ParsedDataVectorUtilities" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_ParsedDataVectorUtilities" end time: Feb 20 00:11 CET
"test_ParsedDataVectorUtilities" time elapsed: 00:00:00
----------------------------------------------------------

92/137 Testing: test_FieldValue
92/137 Test: test_FieldValue
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_FieldValue"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_FieldValue" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_FieldValue" end time: Feb 20 00:11 CET
"test_FieldValue" time elapsed: 00:00:00
----------------------------------------------------------

93/137 Testing: test_TextParser
93/137 Test: test_TextParser
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TextParser"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_TextParser" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_TextParser" end time: Feb 20 00:11 CET
"test_TextParser" time elapsed: 00:00:00
----------------------------------------------------------

94/137 Testing: test_MissileDatcomReader
94/137 Test: test_MissileDatcomReader
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MissileDatcomReader"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_MissileDatcomReader" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_MissileDatcomReader" end time: Feb 20 00:11 CET
"test_MissileDatcomReader" time elapsed: 00:00:00
----------------------------------------------------------

95/137 Testing: test_MissileDatcomData
95/137 Test: test_MissileDatcomData
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MissileDatcomData"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_MissileDatcomData" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_MissileDatcomData" end time: Feb 20 00:11 CET
"test_MissileDatcomData" time elapsed: 00:00:00
----------------------------------------------------------

96/137 Testing: test_DictionaryInputSystem
96/137 Test: test_DictionaryInputSystem
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_DictionaryInputSystem"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_DictionaryInputSystem" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_DictionaryInputSystem" end time: Feb 20 00:11 CET
"test_DictionaryInputSystem" time elapsed: 00:00:00
----------------------------------------------------------

97/137 Testing: test_Extractor
97/137 Test: test_Extractor
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_Extractor"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_Extractor" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_Extractor" end time: Feb 20 00:11 CET
"test_Extractor" time elapsed: 00:00:00
----------------------------------------------------------

98/137 Testing: test_FixedWidthParser
98/137 Test: test_FixedWidthParser
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_FixedWidthParser"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_FixedWidthParser" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_FixedWidthParser" end time: Feb 20 00:11 CET
"test_FixedWidthParser" time elapsed: 00:00:00
----------------------------------------------------------

99/137 Testing: test_SeparatedParser
99/137 Test: test_SeparatedParser
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SeparatedParser"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_SeparatedParser" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_SeparatedParser" end time: Feb 20 00:11 CET
"test_SeparatedParser" time elapsed: 00:00:00
----------------------------------------------------------

100/137 Testing: test_LinearFieldTransform
100/137 Test: test_LinearFieldTransform
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LinearFieldTransform"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_LinearFieldTransform" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_LinearFieldTransform" end time: Feb 20 00:11 CET
"test_LinearFieldTransform" time elapsed: 00:00:00
----------------------------------------------------------

101/137 Testing: test_SolarActivityData
101/137 Test: test_SolarActivityData
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SolarActivityData"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_SolarActivityData" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   1.10 sec
----------------------------------------------------------
Test Passed.
"test_SolarActivityData" end time: Feb 20 00:11 CET
"test_SolarActivityData" time elapsed: 00:00:01
----------------------------------------------------------

102/137 Testing: test_MultiArrayReader
102/137 Test: test_MultiArrayReader
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MultiArrayReader"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_MultiArrayReader" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_MultiArrayReader" end time: Feb 20 00:11 CET
"test_MultiArrayReader" time elapsed: 00:00:00
----------------------------------------------------------

103/137 Testing: test_AerodynamicCoefficientReader
103/137 Test: test_AerodynamicCoefficientReader
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AerodynamicCoefficientReader"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/InputOutput
"test_AerodynamicCoefficientReader" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_AerodynamicCoefficientReader" end time: Feb 20 00:11 CET
"test_AerodynamicCoefficientReader" time elapsed: 00:00:00
----------------------------------------------------------

104/137 Testing: test_MathematicalConstants
104/137 Test: test_MathematicalConstants
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MathematicalConstants"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_MathematicalConstants" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_MathematicalConstants" end time: Feb 20 00:11 CET
"test_MathematicalConstants" time elapsed: 00:00:00
----------------------------------------------------------

105/137 Testing: test_LinearAlgebra
105/137 Test: test_LinearAlgebra
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LinearAlgebra"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_LinearAlgebra" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_LinearAlgebra" end time: Feb 20 00:11 CET
"test_LinearAlgebra" time elapsed: 00:00:00
----------------------------------------------------------

106/137 Testing: test_CoordinateConversions
106/137 Test: test_CoordinateConversions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CoordinateConversions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_CoordinateConversions" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 10 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_CoordinateConversions" end time: Feb 20 00:11 CET
"test_CoordinateConversions" time elapsed: 00:00:00
----------------------------------------------------------

107/137 Testing: test_NearestNeighbourSearch
107/137 Test: test_NearestNeighbourSearch
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_NearestNeighbourSearch"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_NearestNeighbourSearch" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_NearestNeighbourSearch" end time: Feb 20 00:11 CET
"test_NearestNeighbourSearch" time elapsed: 00:00:00
----------------------------------------------------------

108/137 Testing: test_NumericalDerivative
108/137 Test: test_NumericalDerivative
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_NumericalDerivative"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_NumericalDerivative" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_NumericalDerivative" end time: Feb 20 00:11 CET
"test_NumericalDerivative" time elapsed: 00:00:00
----------------------------------------------------------

109/137 Testing: test_LegendrePolynomials
109/137 Test: test_LegendrePolynomials
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LegendrePolynomials"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_LegendrePolynomials" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_LegendrePolynomials" end time: Feb 20 00:11 CET
"test_LegendrePolynomials" time elapsed: 00:00:00
----------------------------------------------------------

110/137 Testing: test_SphericalHarmonics
110/137 Test: test_SphericalHarmonics
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SphericalHarmonics"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_SphericalHarmonics" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_SphericalHarmonics" end time: Feb 20 00:11 CET
"test_SphericalHarmonics" time elapsed: 00:00:00
----------------------------------------------------------

111/137 Testing: test_RotationAboutArbitraryAxis
111/137 Test: test_RotationAboutArbitraryAxis
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RotationAboutArbitraryAxis"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/BasicMathematics
"test_RotationAboutArbitraryAxis" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 5 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_RotationAboutArbitraryAxis" end time: Feb 20 00:11 CET
"test_RotationAboutArbitraryAxis" time elapsed: 00:00:00
----------------------------------------------------------

112/137 Testing: test_LawgsSurfaceGeometry
112/137 Test: test_LawgsSurfaceGeometry
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LawgsSurfaceGeometry"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/GeometricShapes
"test_LawgsSurfaceGeometry" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_LawgsSurfaceGeometry" end time: Feb 20 00:11 CET
"test_LawgsSurfaceGeometry" time elapsed: 00:00:00
----------------------------------------------------------

113/137 Testing: test_CubicSplineInterpolator
113/137 Test: test_CubicSplineInterpolator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_CubicSplineInterpolator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Interpolators
"test_CubicSplineInterpolator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.03 sec
----------------------------------------------------------
Test Passed.
"test_CubicSplineInterpolator" end time: Feb 20 00:11 CET
"test_CubicSplineInterpolator" time elapsed: 00:00:00
----------------------------------------------------------

114/137 Testing: test_HermiteCubicSplineInterpolator
114/137 Test: test_HermiteCubicSplineInterpolator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_HermiteCubicSplineInterpolator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Interpolators
"test_HermiteCubicSplineInterpolator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_HermiteCubicSplineInterpolator" end time: Feb 20 00:11 CET
"test_HermiteCubicSplineInterpolator" time elapsed: 00:00:00
----------------------------------------------------------

115/137 Testing: test_LinearInterpolator
115/137 Test: test_LinearInterpolator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LinearInterpolator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Interpolators
"test_LinearInterpolator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.03 sec
----------------------------------------------------------
Test Passed.
"test_LinearInterpolator" end time: Feb 20 00:11 CET
"test_LinearInterpolator" time elapsed: 00:00:00
----------------------------------------------------------

116/137 Testing: test_MultiLinearInterpolator
116/137 Test: test_MultiLinearInterpolator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MultiLinearInterpolator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Interpolators
"test_MultiLinearInterpolator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_MultiLinearInterpolator" end time: Feb 20 00:11 CET
"test_MultiLinearInterpolator" time elapsed: 00:00:00
----------------------------------------------------------

117/137 Testing: test_LagrangeInterpolator
117/137 Test: test_LagrangeInterpolator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_LagrangeInterpolator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Interpolators
"test_LagrangeInterpolator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_LagrangeInterpolator" end time: Feb 20 00:11 CET
"test_LagrangeInterpolator" time elapsed: 00:00:00
----------------------------------------------------------

118/137 Testing: test_EulerIntegrator
118/137 Test: test_EulerIntegrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_EulerIntegrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_EulerIntegrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_EulerIntegrator" end time: Feb 20 00:11 CET
"test_EulerIntegrator" time elapsed: 00:00:00
----------------------------------------------------------

119/137 Testing: test_NumericalIntegrator
119/137 Test: test_NumericalIntegrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_NumericalIntegrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_NumericalIntegrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_NumericalIntegrator" end time: Feb 20 00:11 CET
"test_NumericalIntegrator" time elapsed: 00:00:00
----------------------------------------------------------

120/137 Testing: test_RungeKutta4Integrator
120/137 Test: test_RungeKutta4Integrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKutta4Integrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKutta4Integrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_RungeKutta4Integrator" end time: Feb 20 00:11 CET
"test_RungeKutta4Integrator" time elapsed: 00:00:00
----------------------------------------------------------

121/137 Testing: test_RungeKuttaVariableStepSizeIntegrator
121/137 Test: test_RungeKuttaVariableStepSizeIntegrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKuttaVariableStepSizeIntegrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKuttaVariableStepSizeIntegrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_RungeKuttaVariableStepSizeIntegrator" end time: Feb 20 00:11 CET
"test_RungeKuttaVariableStepSizeIntegrator" time elapsed: 00:00:00
----------------------------------------------------------

122/137 Testing: test_RungeKuttaCoefficients
122/137 Test: test_RungeKuttaCoefficients
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKuttaCoefficients"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKuttaCoefficients" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_RungeKuttaCoefficients" end time: Feb 20 00:11 CET
"test_RungeKuttaCoefficients" time elapsed: 00:00:00
----------------------------------------------------------

123/137 Testing: test_RungeKuttaFehlberg45Integrator
123/137 Test: test_RungeKuttaFehlberg45Integrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKuttaFehlberg45Integrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKuttaFehlberg45Integrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.02 sec
----------------------------------------------------------
Test Passed.
"test_RungeKuttaFehlberg45Integrator" end time: Feb 20 00:11 CET
"test_RungeKuttaFehlberg45Integrator" time elapsed: 00:00:00
----------------------------------------------------------

124/137 Testing: test_RungeKuttaFehlberg56Integrator
124/137 Test: test_RungeKuttaFehlberg56Integrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKuttaFehlberg56Integrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKuttaFehlberg56Integrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 4 test cases...
/Users/richardcronheim/tudatBundle-rich-cron/tudat/Tudat/Mathematics/NumericalIntegrators/UnitTests/unitTestRungeKuttaFehlberg56Integrator.cpp:100: error in "test_RungeKuttaFehlberg56_Integrator_Fehlberg_Benchmark": check computedError( 1 ) / fehlbergError( 1 ) >= 0.0 failed [-0.23877399296732818 < 0]

*** 1 failure detected in test suite "Master Test Suite"
<end of output>
Test time =   0.03 sec
----------------------------------------------------------
Test Failed.
"test_RungeKuttaFehlberg56Integrator" end time: Feb 20 00:11 CET
"test_RungeKuttaFehlberg56Integrator" time elapsed: 00:00:00
----------------------------------------------------------

125/137 Testing: test_RungeKuttaFehlberg78Integrator
125/137 Test: test_RungeKuttaFehlberg78Integrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKuttaFehlberg78Integrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKuttaFehlberg78Integrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_RungeKuttaFehlberg78Integrator" end time: Feb 20 00:11 CET
"test_RungeKuttaFehlberg78Integrator" time elapsed: 00:00:00
----------------------------------------------------------

126/137 Testing: test_RungeKutta87DormandPrinceIntegrator
126/137 Test: test_RungeKutta87DormandPrinceIntegrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RungeKutta87DormandPrinceIntegrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalIntegrators
"test_RungeKutta87DormandPrinceIntegrator" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_RungeKutta87DormandPrinceIntegrator" end time: Feb 20 00:11 CET
"test_RungeKutta87DormandPrinceIntegrator" time elapsed: 00:00:00
----------------------------------------------------------

127/137 Testing: test_RootFinders
127/137 Test: test_RootFinders
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RootFinders"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/RootFinders
"test_RootFinders" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 19 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_RootFinders" end time: Feb 20 00:11 CET
"test_RootFinders" time elapsed: 00:00:00
----------------------------------------------------------

128/137 Testing: test_SimpleLinearRegression
128/137 Test: test_SimpleLinearRegression
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SimpleLinearRegression"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_SimpleLinearRegression" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 3 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_SimpleLinearRegression" end time: Feb 20 00:11 CET
"test_SimpleLinearRegression" time elapsed: 00:00:00
----------------------------------------------------------

129/137 Testing: test_BasicStatistics
129/137 Test: test_BasicStatistics
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_BasicStatistics"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_BasicStatistics" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.00 sec
----------------------------------------------------------
Test Passed.
"test_BasicStatistics" end time: Feb 20 00:11 CET
"test_BasicStatistics" time elapsed: 00:00:00
----------------------------------------------------------

130/137 Testing: test_MultiVariateProbabilityDistributions
130/137 Test: test_MultiVariateProbabilityDistributions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_MultiVariateProbabilityDistributions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_MultiVariateProbabilityDistributions" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.02 sec
----------------------------------------------------------
Test Passed.
"test_MultiVariateProbabilityDistributions" end time: Feb 20 00:11 CET
"test_MultiVariateProbabilityDistributions" time elapsed: 00:00:00
----------------------------------------------------------

131/137 Testing: test_BoostDistributions
131/137 Test: test_BoostDistributions
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_BoostDistributions"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_BoostDistributions" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 1 test case...

*** No errors detected
<end of output>
Test time =   0.01 sec
----------------------------------------------------------
Test Passed.
"test_BoostDistributions" end time: Feb 20 00:11 CET
"test_BoostDistributions" time elapsed: 00:00:00
----------------------------------------------------------

132/137 Testing: test_KernelDensityDistribution
132/137 Test: test_KernelDensityDistribution
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_KernelDensityDistribution"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_KernelDensityDistribution" start time: Feb 20 00:11 CET
Output:
----------------------------------------------------------
Running 7 test cases...

*** No errors detected
<end of output>
Test time =   3.30 sec
----------------------------------------------------------
Test Passed.
"test_KernelDensityDistribution" end time: Feb 20 00:12 CET
"test_KernelDensityDistribution" time elapsed: 00:00:03
----------------------------------------------------------

133/137 Testing: test_RandomSampling
133/137 Test: test_RandomSampling
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_RandomSampling"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/Statistics
"test_RandomSampling" start time: Feb 20 00:12 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   1.26 sec
----------------------------------------------------------
Test Passed.
"test_RandomSampling" end time: Feb 20 00:12 CET
"test_RandomSampling" time elapsed: 00:00:01
----------------------------------------------------------

134/137 Testing: test_TrapezoidalIntegrator
134/137 Test: test_TrapezoidalIntegrator
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_TrapezoidalIntegrator"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/Mathematics/NumericalQuadrature
"test_TrapezoidalIntegrator" start time: Feb 20 00:12 CET
Output:
----------------------------------------------------------
Running 2 test cases...

*** No errors detected
<end of output>
Test time =   0.08 sec
----------------------------------------------------------
Test Passed.
"test_TrapezoidalIntegrator" end time: Feb 20 00:12 CET
"test_TrapezoidalIntegrator" time elapsed: 00:00:00
----------------------------------------------------------

135/137 Testing: test_SpiceInterface
135/137 Test: test_SpiceInterface
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_SpiceInterface"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/External/SpiceInterface
"test_SpiceInterface" start time: Feb 20 00:12 CET
Output:
----------------------------------------------------------
Running 7 test cases...

*** No errors detected
<end of output>
Test time =   0.13 sec
----------------------------------------------------------
Test Passed.
"test_SpiceInterface" end time: Feb 20 00:12 CET
"test_SpiceInterface" time elapsed: 00:00:00
----------------------------------------------------------

136/137 Testing: test_EnvironmentSetup
136/137 Test: test_EnvironmentSetup
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_EnvironmentSetup"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/SimulationSetup
"test_EnvironmentSetup" start time: Feb 20 00:12 CET
Output:
----------------------------------------------------------
Running 9 test cases...

*** No errors detected
<end of output>
Test time =   3.05 sec
----------------------------------------------------------
Test Passed.
"test_EnvironmentSetup" end time: Feb 20 00:12 CET
"test_EnvironmentSetup" time elapsed: 00:00:03
----------------------------------------------------------

137/137 Testing: test_AccelerationModelSetup
137/137 Test: test_AccelerationModelSetup
Command: "/Users/richardcronheim/tudatBundle-rich-cron/tudat/bin/unit_tests/test_AccelerationModelSetup"
Directory: /Users/richardcronheim/build-tudatBundle-rich-cron-Desktop-Default/tudat/Tudat/SimulationSetup
"test_AccelerationModelSetup" start time: Feb 20 00:12 CET
Output:
----------------------------------------------------------
Running 5 test cases...
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator
Warning, overriding existing bank angle function in AerodynamicAngleCalculator
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator
Warning, overriding existing bank angle function in AerodynamicAngleCalculator
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator
Warning, overriding existing bank angle function in AerodynamicAngleCalculator
Warning, overriding existing angle of attack function in AerodynamicAngleCalculator
Warning, overriding existing angle of sideslip function in AerodynamicAngleCalculator
Warning, overriding existing bank angle function in AerodynamicAngleCalculator

*** No errors detected
<end of output>
Test time =   0.31 sec
----------------------------------------------------------
Test Passed.
"test_AccelerationModelSetup" end time: Feb 20 00:12 CET
"test_AccelerationModelSetup" time elapsed: 00:00:00
----------------------------------------------------------

End testing: Feb 20 00:12 CET

[DominicDirkx]

Thanks for bringing this to our attention. Neither of the two seems to be any cause for concern, so go ahead with the assignments. We're already working on one of the problems (Cowell state derivative), for which we hope to have more information by the end of the week.

As no one else has reported the RKF56 issue yet, we may ask you to drop by the office hours so we can have a better look, in case we cannot get to the bottom of it from just the error report.