Model reference single stage digital adaptive flight controller development
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Authors
Alag, Gurbux S.
Issue Date
1976-05
Type
Electronic thesis
Thesis
Thesis
Language
ENG
Keywords
Electrical Systems engineering
Alternative Title
Abstract
Adaptive flight control systems are of interest because of their potential for providing uniform stability and handling qualities over a wide flight envelope despite uncertainties in the open loop characteristics of the aircraft. Because of the attractiveness of adaptive control and the availability of digital flight computers, a study has been made in order to define an implementable digital adaptive control system which can be used for a typical fighter aircraft.
Description
May 1976
School of Engineering
School of Engineering
Full Citation
Publisher
Rensselaer Polytechnic Institute, Troy, NY