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Application of a passivity based control methodology for flexible joint robots to a simplified Space Shuttle RMSA passivity approach for the control design of flexible joint robots is applied to the rate control of a three-link arm modeled after the shoulder yaw joint of the Space Shuttle Remote Manipulator System (RMS). The system model includes friction and elastic joint couplings modeled as nonlinear springs. The basic structure of the proposed controller is the sum of a model-based feedforward and a model-independent feedback. A regulator approach with link state feedback is employed to define the desired motor state. Passivity theory is used to design a motor state-based controller to stabilize the error system formed by the feedforward. Simulation results show that greatly improved performance was obtained by using the proposed controller over the existing RMS controller.
Document ID
19930038900
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sicard, Pierre
(NASA Headquarters Washington, DC United States)
Wen, John T.
(NASA Center for Intelligent Robotic Systems for Space Exploration; Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: 1992 American Control Conference, 11th, Chicago, IL, June 24-26, 1992, Proceedings. Vol. 2 (A93-22776 07-63)
Publisher: Institute of Electrical and Electronics Engineers
Subject Category
Cybernetics
Accession Number
93A22897
Distribution Limits
Public
Copyright
Other

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