A source of space station attitude disturbances is identified. The attitude disturbance is driven by internal space station motions and is a direct result of conservation of angular momentum. Three examples are used to illustrate the effect: a planar three link system, a rigid carrier body with two moveable masses, and a nonplanar five link system. Simulation results are given to show the magnitude of the attitude change in each example. Factors which accentuate or attenuate this disturbance effect are discussed.
Space station attitude disturbance arising from internal motions
American Control Conference ; 1993 ; Ann Arbor, MI, United States
1993-06-03
Aufsatz (Konferenz)
Keine Angabe
Englisch
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