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Mixed H2/H-Infinity Control of a Flexible Space StructureAs theory progresses for design and analysis of robust multivariable control laws, synthesis procedures and to a larger extent, experimental verification generally lags behind. Recent developments in robust control theory have extended the H-infinity and mu-synthesis methods to incorporate H2 properties in the control synthesis. A major difficulty in implementing robust controllers is the order of the compensator and associated complexity of the computation required for synthesis, especially when order constraints are imposed. This paper presents results of system identification and robust control design for the Controls/Structures Interaction Ground Test Facility at NASA/Marshall Space Flight Center.
Document ID
19990054826
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Whorton, Mark
(NASA Marshall Space Flight Center Huntsville, AL United States)
Calise, Anthony J.
(Georgia Inst. of Tech. Atlanta, GA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1997
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Guidance, Navigation and Control
Location: New Orleans, LA
Country: United States
Start Date: August 11, 1997
End Date: August 13, 1997
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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