Response relations, vehicle attitude, control torque, wheel motion, mechanical power, and energy consumption for space vehicle subjected to sinusoidal or impulsive disturbances; resulting normalized numerical relations serve as order of magnitude basis for preliminary design estimates and comparisons; response relations are derived for single axis model; applicability to 3-axis design; control system proposed decouples vehicle dynamics so that motions are exactly single axis.
Some basic response relations for reaction-wheel attitude control
ARS J
ARS Journal ; 32 , n 1 ; p 61-74
1962
14 pages
Article (Journal)
English
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