The feasibility of providing active damping augmentation of the Space Shuttle Remote Manipulator System (RMS) following normal payload-handling operations is investigated. The approach used in the analysis is described and the results from both linear and nonlinear performance analyses of candidate laws are presented, demonstrating that significant improvement in the RMS dynamic response can be achieved through active control using measured RMS tip acceleration data for feedback.
Active vibration damping of the Space Shuttle Remote Manipulator System
AIAA Guidance, Navigation and Control Conference ; 1991 ; New Orleans, LA, United States
1991-01-01
Conference paper
No indication
English
Active Vibration Damping of the Space Shuttle Remote Manipulator System
Online Contents | 1993
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