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Low Bandwidth Robust Controllers for FlightThrough throttle manipulations, engine thrust can be used for emergency flight control for multi-engine aircraft. Previous study by NASA Dryden has shown the use of throttles for emergency flight control to be very difficult. In general, manual fly-by-throttle is extremely difficult - with landing almost impossible, but control augmentation makes runway landings feasible. Flight path control using throttles-only to achieve safe emergency landing for a large jet transport airplane, Boeing 720, was investigated using Quantitative Feedback Theory (QFT). Results were compared to an augmented control developed in a previous simulation study. The control augmentation corrected the unsatisfactory open-loop characteristics by increasing system bandwidth and damping, but increasing the control bandwidth substantially proved very difficult. The augmented pitch control is robust under no or moderate turbulence. The augmented roll control is sensitive to configuration changes.
Document ID
19960054339
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biezad, Daniel J.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Chou, Hwei-Lan
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-202406
NAS 1.26:202406
Report Number: NASA-CR-202406
Report Number: NAS 1.26:202406
Accession Number
96N36513
Funding Number(s)
CONTRACT_GRANT: NCC2-811
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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