Hello,
I have been working with the Python API and have encountered a roadblock.
So far, I have been able to run the propagation of a satellite with a set
force model, but I would like to expand upon this. Currently I am trying to
implement two impulsive burns, so I can change the orbit of a satel
Hello,
Using the python API to run a mission with a Spacecraft and an
ImpulsiveBurn results in the following API exception
~/gmat-git/application/bin/gmatpy/gmat_py.py in Initialize(*args)
23606 23607 def Initialize(*args):> 23608 return
_gmat_py.Initialize(*args) 23609 23610 def Clear(*
