Command equation for inertia wheel control system which results in desirable dynamic response and precise control is derived; three degree of freedom study indicates that inertia coupling and precession coupling have only small effects on results; single degree of freedom bench tests verified dynamic response predicted and demonstrated control within plus or minus 9 arc-sec of reference attitude.
Satellite attitude control using combination of inertia wheels and bar magnet
NASA -- Tech Note
1960
42 pages
Report
English
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Study of systems using inertia wheels for precise attitude control of satellite
Engineering Index Backfile | 1961
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