First commit adding support for orbital maneuvers changing argument of periapsis #66
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…f periapsis Also changing float-casting of argument of acos for true anomaly calculation to only happen if a NaN is thrown under normal double-precision calculations Added demonstration of argument of periapsis change maneuver to example simulation workflow file
Removing offset print statement
Cleaning up some commented out code
Attempting to debug failed tests in Github actions workflow
More bugfixing for isnan call
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Context
I wanted to build in support for another example of an orbital maneuver, so I chose maneuvers to change the argument of periapsis of a satellite's orbit. This was interesting because it requires non-constant thrust direction.
Changes
Testing
Needs to pass existing test suites