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Minimum-size design of regulation systems and the application to Space StationA method is proposed to determine the sizes of the regulator and observer and to design the feedback and Kalman gain matrices for the reduced system. The sizes determined are minimum in the sense of satisfying the specified eigenvalue limits when the interaction between the regulator and the observer can be neglected. The resulting sizes will depend on the properties of the original system and the desired response. If the interaction between the regulator and the observer becomes substantial, more modes in the observer should be included, or other methods should be used for reducing the observation spillover or control spillover.
Document ID
19910071204
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reddy, A. S. S. R.
(City College New York, United States)
Ruan, Mifang
(City Coll. of the City Univ. of New York NY, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 89-630
Report Number: AAS PAPER 89-630
Accession Number
91A55827
Distribution Limits
Public
Copyright
Other

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