Celestial Body Orientation

General help that does not fall into a more specific category

Celestial Body Orientation

Postby kdrozd » Sun Nov 01, 2015 8:16 pm

When a new body, such as an asteroid, is being added into a GMAT mission there are three parameters I would like confirmation on what they are. Those three parameters are the spin axis RA constant, spin axis DEC constant, and the rotation constant. I think those parameters are the pole position (J200 RA/DEC) and the location of the prime meridian (epoch J200) respectively. Is this correct?
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