Mathematical model of bang-bang reaction jet attitude control system, capable of generating high moments in space vehicle, is derived on basis of conditional switching techniques; computer study of system was accomplished and its actual vs theoretical performance compared; study showed that model yields desired attitude change in minimum amount of time; parameter study was made to derive magnitude of moments, duty cycle, angular impulse, and dynamic response information.
Bang-bang attitude control system for space vehicles
Aerospace Eng
Aerospace Engineering ; 21 , n 10
1962
Article (Journal)
English
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