Open GoogleCodeExporter opened 9 years ago
It's kind of tricky .. in the code, a Structure (spacecraft) is made of
Modules, and
each Module has an offset, size, and mass (among other things). The
center-of-mass
can be determined by averaging (offset*mass), and the moment of inertia is
currently
modeled as a cylinder based on the maximum dimensions of the spacecraft (see
...exo.orbit.ship.Structure.getIntertiaVector() and computeCenterOfMass()).
Certainly
it could be better with each module having its own moment of intertia.
Original comment by seh...@gmail.com
on 24 Apr 2008 at 2:42
You should have an option to just plug in a known value. Some of the historical
spacecraft have the values for their configuration listed so you don't have to
guess.
Original comment by robertsc...@gmail.com
on 24 Apr 2008 at 2:42
Also one reason I posted this is because when I tried the gemini it seemed too
responsive on the reaction control thrusters compared to my orbiter add-on
which uses
the historical values.
Original comment by robertsc...@gmail.com
on 24 Apr 2008 at 2:45
Original issue reported on code.google.com by
robertsc...@gmail.com
on 17 Apr 2008 at 8:29