DocumentCode
2103130
Title
Taking H∞ control into flight
Author
Hyde, R.A. ; Glover, K.
Author_Institution
Dept. of Eng., Cambridge Univ., UK
fYear
1993
fDate
15-17 Dec 1993
Firstpage
1458
Abstract
A flight control law for the longitudinal motion of a Harrier jump jet has been developed using H∞ techniques. Linear design is carried out using loop shaping of the plant, and robustness is achieved using normalised coprime factors. Implementation issues such as gain scheduling and actuator saturations for multivariable H∞ controllers have been addressed. Results of piloted simulation on the Defence Research Agency advanced flight simulator are given. The control law provides a demonstrator for the application of H∞ techniques to a real control problem. The Harrier application is particularly interesting because of the use of vectored thrust. Many of the design problems encountered may therefore be relevant to the recent interest in using limited authority vectored thrust for manoeuvre enhancement
Keywords
aircraft control; attitude control; closed loop systems; control system synthesis; multivariable control systems; optimal control; Defence Research Agency; H∞ control; Harrier jump jet; actuator saturations; advanced flight simulator; closed loop control; flight control; gain scheduling; longitudinal motion; loop shaping; multivariable H∞ controllers; normalised coprime factors; robustness; Actuators; Aerospace control; Aerospace simulation; Aircraft; Attitude control; Design methodology; H infinity control; Motion control; Robustness; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location
San Antonio, TX
Print_ISBN
0-7803-1298-8
Type
conf
DOI
10.1109/CDC.1993.325429
Filename
325429
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