Aeronautics and astronautics
Spacecraft
Attitude control
Inventor
active
Controlled-emission solar tabs for attitude solar sailing
Correction of spacecraft steering control law for unexpected...
Method of controlling attitude of a momentum biased...
Momentum unloading using gimbaled thrusters
Nutation sensor and nutation control system for a dual-spin stab
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Profile ID: LFUS-PAI-P-1299975