The GUI is a simple earth orbit transfer planner the user starts with an initial orbit and have to suggest a sequence from propagation, maneuver or a target state vector to optimize for.
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the code is utilizing genetic algorithms to satisfy the target orbit requirements and the user can change the GA parameters and the tolerance through the setting panel and there's an option to make an orbital rendez-vous after reaching the final orbit.
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The inputs:
user have to start with an initial orbit state vector
the planing inputs:
propagation:
specify propagation time.
Maneuver:
first choose maneuver type
Target:
final orbit targeted to optimize the transfer