NASA NTRS · 19910052975
Identification of pilot-vehicle dynamics from simulation and flight test
Abstract
The 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.
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Hess, Ronald A.. 1990-01-01. Identification of pilot-vehicle dynamics from simulation and flight test. https://ntrs.nasa.gov/citations/19910052975
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