DocumentCode
2767637
Title
Robust integrated flight and propulsion control (IFPC) of an experimental STOVL aircraft
Author
Bates, D.G. ; Gatley, S.L. ; Postlethwaite, I. ; Gillett, L. ; Littleboy, D.
Author_Institution
Dept. of Eng., Leicester Univ., UK
Volume
4
fYear
1998
fDate
16-18 Dec 1998
Firstpage
4220
Abstract
The technique of ℋ∞ loop-shaping is used to design a robust integrated flight and propulsion controller for an experimental STOVL aircraft configuration, based on the Harrier T.Mk 10 airframe with a Rolls Royce Spey engine. Performance properties of the integrated controller are validated via nonlinear simulation
Keywords
H∞ control; aerospace propulsion; aircraft control; control system synthesis; military aircraft; robust control; H∞ control; Harrier T.Mk 10 airframe; Rolls Royce Spey engine; STOVL aircraft; flight and propulsion control; loop-shaping; propulsion control; robust control; Aerospace control; Aerospace engineering; Aircraft propulsion; Blades; Control system synthesis; Control systems; Engines; Fuels; Robust control; Thermodynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.761965
Filename
761965
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