Various possible systems are examined for suitability and 3, which appear more promising, are analyzed using Orbiting Astronomical Observatory as example; system which uses error rate network to provide damping is superior to other two; dynamic tracking error of less than plus or minus 0.5 sec of arc was obtained.
Study of systems using inertia wheels for precise attitude control of satellite
NASA -- Tech Note
1961
71 pages
Report
English
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Satellite attitude control using combination of inertia wheels and bar magnet
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