Attitude propagation tests

Conversations pertaining to the testing of GMAT

Attitude propagation tests

Postby JTichy » Tue Jun 16, 2009 1:32 pm

Spacecraft with attitude needs to be propagated with varying force models and test against COTS software tools for accuracy. A COTS software tool needs to be selected which accurately reflects the methods used by GMAT for attitude propagation.

Test should include;

Local and Custom Defined Coordinate Systems
All available force model objects
Planetary and Heliocentric Orbits
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