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Sensitivity of Space Station Alpha Joint robust controller to structural modal parameter variationsThe baseline design of the photovoltaic-array sun-tracking control system is presented with special attention given to the optimization of design variables related to stability and performance. The procedures utilized to attenuate control/structure interaction are described, and controller sensitivity to variations in structural modal parameters is examined. Constrained optimization techniques determine the stability margin and tracking capability, which are then tested for sensitivity to variations in natural frequency, mode-shape amplitudes, and modal-damping ratios. The effect of variations in the modal parameters of the dominant modes on performance indicators is also examined to optimize tracking-performance responsiveness and satisfy the design requirements. It is concluded that accurate on-orbit modal data are necessary to make the reoptimization procedure effective in improving the performance of the control system.
Document ID
19910065013
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kumar, Renjith R.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Cooper, Paul A.
(NASA Langley Research Center Hampton, VA, United States)
Lim, Tae W.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 91-2665
Report Number: AIAA PAPER 91-2665
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
91A49636
Distribution Limits
Public
Copyright
Other

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