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On the use of distributed sensing in control of large flexible spacecraftDistributed processing technology is being developed to process signals from distributed sensors using distributed computations. Thiw work presents a scheme for calculating the operators required to emulate a conventional Kalman filter and regulator using such a computer. The scheme makes use of conventional Kalman theory as applied to the control of large flexible structures. The required computation of the distributed operators given the conventional Kalman filter and regulator is explained. A straightforward application of this scheme may lead to nonsmooth operators whose convergence is not apparent. This is illustrated by application to the Mini-Mast, a large flexible truss at the Langley Research Center used for research in structural dynamics and control. Techniques for developing smooth operators are presented. These involve spatial filtering as well as adjusting the design constants in the Kalman theory. Results are presented that illustrate the degree of smoothness achieved.
Document ID
19920069368
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, Raymond C.
(NASA Langley Research Center Hampton, VA, United States)
Ghosh, Dave
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: ASME Winter Annual Meeting
Location: Dallas, TX
Country: United States
Start Date: November 25, 1990
End Date: November 30, 1990
Sponsors: ASME
Accession Number
92A51992
Distribution Limits
Public
Copyright
Other

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