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A practical scheme for adaptive aircraft flight control systemsA flight control system design is presented, that can be implemented by analog hardware, to be used to control an aircraft with uncertain parameters. The design is based upon the use of modern control theory. The ideas are illustrated by considering control of STOL longitudinal dynamics.
Document ID
19740017475
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Athans, M. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Willner, D. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Publication Information
Publication: NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing
Subject Category
Aircraft
Accession Number
74N25588
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-2273-72
CONTRACT_GRANT: NGL-22-009-124
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19740017456Collected WorksParameter estimation techniques and application in aircraft flight testing
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