Paper considers constraints affecting choice of basic attitude control system to be used and tradeoffs in selection, sizing, and mode of operation of components with which it may be implemented; primary characteristics of techniques and hardware are classified according to characteristic requirements; examples are drawn from existing spacecraft; systems under development are also considered.
General considerations in selection of attitude control systems
SAE-NASA -- Proc
Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
21 pages
Conference paper
English
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General Considerations in the Selection of Attitude Control Systems
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