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Robust fixed order dynamic compensation for large space structure controlA simple formulation for designing fixed order dynamic compensators which are robust to both uncertainty at the plant input and structured uncertainty in the plant dynamics is presented. The emphasis is on designing low order compensators for systems of high order. The formulation is done in an output feedback setting which exploits an observer canonical form to represent the compensator dynamics. The formulation also precludes the use of direct feedback of the plant output. The main contribution lies in defining a method for penalizing the states of the plant and of the compensator, and for choosing the distribution on initial conditions so that the loop transfer matrix approximates that of a full state design. To improve robustness to parameter uncertainty, the formulation avoids the introduction of sensitivity states, which has led to complex formulations in earlier studies where only structured uncertainty has been considered.
Document ID
19900013743
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Calise, Anthony J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Byrns, Edward V., Jr.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
December 15, 1989
Publication Information
Publication: Jet Propulsion Lab., California Inst. of Tech., Proceedings of the 3rd Annual Conference on Aerospace Computational Control, Volume 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N23059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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