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Robust stabilization of the Space Station in the presence of inertia matrix uncertaintyThis paper presents a robust H-infinity full-state feedback control synthesis method for uncertain systems with D11 not equal to 0. The method is applied to the robust stabilization problem of the Space Station in the face of inertia matrix uncertainty. The control design objective is to find a robust controller that yields the largest stable hypercube in uncertain parameter space, while satisfying the nominal performance requirements. The significance of employing an uncertain plant model with D11 not equal 0 is demonstrated.
Document ID
19930067398
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wie, Bong
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Liu, Qiang
(Arizona State Univ. Tempe, United States)
Sunkel, John
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 2 (A93-51301 22-63)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 93-3803
Accession Number
93A51395
Distribution Limits
Public
Copyright
Other

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