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Decomposition and state variable feedback control of elastic robotic systemsEnergy-efficient, lightweight robot arms for space applications have considerable structural flexibility. An approach to control of a class of flexible robotic systems is presented. A control law is derived which decouples the joint-angle motion from the flexible motion and, in addition, asymptotically decomposes the elastic dynamics into two subsystems. This allows the design of an elastic mode stabilizer independently based on lower order models representing structural flexibility. The closed-loop system is shown to be globally asymptotically stable and robust to uncertaintly in system parameters. Simulation results show that the combination of nonlinear decoupling and elastic stabilization permits rapid, accurate tracking of large joint angle commands with well damped elastic response, in spite of space vehicle motion and payload uncertainty.
Document ID
19850053829
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Singh, S. N.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Schy, A. A.
(NASA Langley Research Center Spacecraft Control Branch, Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Subject Category
Cybernetics
Accession Number
85A35980
Distribution Limits
Public
Copyright
Other

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