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CSI, optimal control, and accelerometers: Trials and tribulationsNew results concerning optimal design with accelerometers are presented. These results show that the designer must be concerned with the stability properties of two Linear Quadratic Gaussian (LQG) compensators, one of which does not explicitly appear in the closed-loop system dynamics. The new concepts of virtual and implemented compensators are introduced to cope with these subtleties. The virtual compensator appears in the closed-loop system dynamics and the implemented compensator appears in control electronics. The stability of one compensator does not guarantee the stability of the other. For strongly stable (robust) systems, both compensators should be stable. The presence of controlled and uncontrolled modes in the system results in two additional forms of the compensator with corresponding terms that are of like form, but opposite sign, making simultaneous stabilization of both the virtual and implemented compensator difficult. A new design algorithm termed sensor augmentation is developed that aids stabilization of these compensator forms by incorporating a static augmentation term associated with the uncontrolled modes in the design process.
Document ID
19940031381
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benjamin, Brian J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Sesak, John R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Publication Information
Publication: NASA. Langley Research Center, NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems
Subject Category
Computer Programming And Software
Accession Number
94N35888
Funding Number(s)
CONTRACT_GRANT: NAS1-19241
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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