Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1996-06-05
1999-09-28
Mojica, Virna Lissi
Aeronautics and astronautics
Spacecraft
Attitude control
244164, 244170, B64G 132, B64G 124
Patent
active
059574100
ABSTRACT:
A low earth orbiting satellite control arrangement according to the invention has an earth sensor for measuring roll and pitch of the satellite relative to an earth oriented moving reference system, a spin wheel mounted along an axis perpendicular to the orbital plane of the satellite for measuring spin of the satellite, and two magnet coils for generating control. A first of the two magnet coils is aligned substantially in parallel to a roll axis of the satellite, and the second is aligned substantially parallel to the yaw axis. Alternative control algorithms are disclosed for controlling attitude, nutation and spin of the satellite based on information from the earth sensor, spin wheel and an observer which is also mounted on the satellite.
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"Magnetic Attitude Control System for Spinning Small Spacecraft", 4th AIAA/USU Meeting, Aug. 27, 1990, Logan 2 (1990).
Bruederle Ernst
Fichter Walter
Surauer Michael
Daimler-Benz Aerospace AG
Mojica Virna Lissi
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