The paper discusses the pointing and stability requirements of the individual experiments on board the Space Shuttle Orbiter, and describes the general features of certain solutions proposed for meeting these requirements. The Instrument Pointing Control Subsystem is examined, and its attitude control system is discussed.
Control requirements of the Shuttle experiments
Symposium on Automatic Control in Space ; 1976 ; Rottach-Egern, Germany
01.01.1976
Sonstige
Keine Angabe
Englisch
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