The dynamics of a zero-momentum three-axis attitude controlled satellite is used to formulate an optimal control problem, which is then solved for the special case where the flywheels operate in a nonsaturating mode. The results then serve as guidelines in the design of simple open-loop and feedback controllers.
Nonsaturating Satellite Open-Loop Feedback Controls
IEEE Transactions on Aerospace and Electronic Systems ; AES-15 , 2 ; 199-203
1979-03-01
1166695 byte
Article (Journal)
Electronic Resource
English
Nonsaturating satellite open-loop feedback controls
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