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Control of SCOLEA relatively low order model is used to control SCOLE. Drastic truncation of the discretized model is proposed by means of a modal expansion. An open loop eigenvalue problem is illustrated as is truncated modal equations, modal state equations, actual output vector and modal Kalman filter. Also illustrated is independent modal-space control.
Document ID
19870008399
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meirovitch, L. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Norris, M. A. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Langley Research Center Proceedings of the 3rd Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17832
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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