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Investigation of an automatic trim algorithm for restructurable aircraft controlThis paper develops and solves an automatic trim problem for restructurable aircraft control. The trim solution is applied as a feed-forward control to reject measurable disturbances following control element failures. Disturbance rejection and command following performances are recovered through the automatic feedback control redesign procedure described by Looze et al. (1985). For this project the existence of a failure detection mechanism is assumed, and methods to cope with potential detection and identification inaccuracies are addressed.
Document ID
19870029493
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weiss, J.
(Alphatech, Inc. Burlington, MA, United States)
Eterno, J.
(Alphatech, Inc. Burlington, MA, United States)
Grunberg, D.
(Alphatech, Inc. Burlington, MA, United States)
Looze, D.
(Alphatech, Inc. Burlington, MA, United States)
Ostroff, A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Stability And Control
Accession Number
87A16767
Funding Number(s)
CONTRACT_GRANT: NAS1-17411
Distribution Limits
Public
Copyright
Other

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