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.
Study of the Space Station Freedom Response to the Disturbance Environment
1994
16 pages
Report
No indication
English
A Study of the Space Station `Freedom' Response to the Disturbance Environment (AAS 93-643)
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