The following topics are discussed: (1) modeling of articulated spacecraft as multi-flex-body systems; (2) nonlinear attitude control by adaptive partial feedback linearizing (PFL) control; (3) attitude dynamics and control for SSF/MRMS; and (4) performance analysis results for attitude control of SSF/MRMS.
Case Study in Nonlinear Dynamics and Control of Articulated Spacecraft: The Space Station Freedom with a Mobile Remote Manipulator System
1994
18 pages
Report
No indication
English
British Library Conference Proceedings | 1994
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