This paper describes the theory of spin signature removal and the results obtained during the Genesis and Contour missions, during which spin axis pointing measurement errors of 1 degree or less were achieved.
Doppler aided attitude determination for spin stabilized spacecraft
13th AAS/AIAA Space Flight Mechanics Meeting
2003-02-09
Conference paper
No indication
English
Magnetometer-Based Attitude Determination for Deployed Spin-Stabilized Spacecraft
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