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Identification of pilot-vehicle dynamics from simulation and flight testThe paper discusses an identification problem in which a basic feedback control structure, or pilot control strategy, is hypothesized. Identification algorithms are employed to determine the particular form of pilot equalization in each feedback loop. It was found that both frequency- and time-domain identification techniques provide useful information.
Document ID
19910052975
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hess, Ronald A.
(California, University Davis, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Stability And Control
Accession Number
91A37598
Distribution Limits
Public
Copyright
Other

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