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Comparison of closed loop model with flight test resultsAn analytic technique capable of predicting the landing characteristics of proposed aircraft configurations in the early stages of design was developed. In this analysis, a linear pilot-aircraft closed loop model was evaluated using experimental data generated with the NT-33 variable stability in-flight simulator. The pilot dynamics are modeled as inner and outer servo loop closures around aircraft pitch attitude, and altitude rate-of-change respectively. The landing flare maneuver is of particular interest as recent experience with military and other highly augmented vehicles shows this task to be relatively demanding, and potentially a critical design point. A unique feature of the pilot model is the incorporation of an internal model of the pilot's desired flight path for the flare maneuver.
Document ID
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
George, F. L.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Date Acquired
August 10, 2013
Publication Date
October 15, 1981
Publication Information
Publication: JPL Proc. of the 17th Ann. Conf. on Manual Control
Subject Category
Man/System Technology And Life Support
Accession Number
Distribution Limits
Work of the US Gov. Public Use Permitted.
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