NASA NTRS · 19820000301
Minimizing Vibrations While Orienting Large Structures
Abstract
Attitute error and error rate minimized by properly-designed control law. Control thrustor returns attitude to point within control dead band whenever attitude error or error rate strays outside. Within dead band, attitude drifts under environmental torque. Leftward thrustor fires when system phase point is to right of error dead band. Opposite is case for rightward thrustor.
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Austin, F.. 1983-05-01. Minimizing Vibrations While Orienting Large Structures. https://ntrs.nasa.gov/citations/19820000301
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