Closes the loop between orbit controller and dynamics model
Summary of Changes
Does this by directly writing the desired impulse calculated by the orbit controller to the impulse field in the dynamics model when it is time to fire thrusters
Enables the plotting of the relative distance and speed of the satellites as well as cumulative delta-V over time
Testing
The plots of relative distance, relative speed, and cumulative delta-V are attached below. From these, it can be seen that the satellites rendezvous.
Closes the loop between orbit controller and dynamics model
Summary of Changes
Testing
The plots of relative distance, relative speed, and cumulative delta-V are attached below. From these, it can be seen that the satellites rendezvous.