A relatively general formulation for studying the dynamics and control of an arbitrary spacecraft with interconnected flexible bodies has been developed. This self-contained and comprehensive numerical algorithm using system modes is applicable to a large class of spacecraft configurations of contemporary and future interest. Here, versatility of the approach is demonstrated through the dynamics and control studies aimed at the evolving Space Station Freedom.
A study of the Space Station Freedom response to the disturbance environment
1994-02-01
Conference paper
No indication
English
A Study of the Space Station `Freedom' Response to the Disturbance Environment (AAS 93-643)
British Library Conference Proceedings | 1993
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