Requirements for three-axis system for satellites; one-axis system proposed uses expulsion charges to compensate for initial disturbance; final fine control exerted by low power flywheel reaction type servo system; it is shown how system can be stabilized without direct derivatives of attitude information; therefore, system also supports stabilization when manually controlled.
Attitude control system for space vehicles
ARS -- J
ARS Journal ; 29 , n 3
1959
5 pages
Aufsatz (Zeitschrift)
Englisch
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Attitude control for space vehicles
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