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Insensitive control technology developmentTHe investigation of two insensitive controller synthesis techniques was reported. The finite dimensional inverse approach produces a time varying insensitive controller and/or parameter identifier by constructing inverse functions derived from a finite number of input output pair relationships. The MD/IM concept relies on the information matrix theory that was developed in the estimation and identification field. The MD/IM synthesis technique is based on the hypothesis that minimizing the information matrix will reduce system identifiability and consequently system sensitivity to uncertain parameters. The controllers designed with both techniques were evaluated on a realistic C-5A aircraft flight control problem. Results indicate that the FDI controller is more suited to trajectory type problems because of its time varying nature. The MD/IM controller performed as well as the top-rated controllers of the initial effort and has direct application to aircraft flight control problems.
Document ID
19780012884
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harvey, C. A.
(Honeywell, Inc. Minneapolis, MN, United States)
Pope, R. E.
(Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1978
Subject Category
Cybernetics
Report/Patent Number
HONEYWELL-77SRC58
NASA-CR-2947
Report Number: HONEYWELL-77SRC58
Report Number: NASA-CR-2947
Accession Number
78N20827
Funding Number(s)
CONTRACT_GRANT: NAS1-14476
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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