DocumentCode
278454
Title
Weighting function specification in H∞ design [battlefield helicopter]
Author
Kellett, M.G. ; White, B A
Author_Institution
R. Mil. Coll. of Sci., Shrivenham, UK
fYear
1991
fDate
33401
Firstpage
42461
Lastpage
42467
Abstract
This paper describes the application of H ∞ to the design of a controller for a battlefield helicopter. It shows the effect of the choice of the weighting functions on the performance of the resulting closed loop system, and indicates how to utilise the freedom of choice. The appropriate handling qualities requirements documents describe the response shapes that are desirable for particular flight conditions, and these can be used as guidelines for further development of the cost function weights. Bandwidths on selected channels can be manipulated to a certain extent by moving the sensitivity function weights, and overshoots can be corrected by careful targeting of the rate feedback channel weights. Actuator movements can be monitored by examining time responses, and these give useful indicators of the feasibility of any design changes
Keywords
aircraft control; control system synthesis; helicopters; military equipment; optimal control; stability; H∞ design; actuator movement monitoring; battlefield helicopter; channel bandwidth manipulation; closed loop system; control design; cost function weights; handling qualities requirements; overshoot correction; rate feedback channel weights; response shapes; sensitivity function weights; time responses; weighting function specification;
fLanguage
English
Publisher
iet
Conference_Titel
Practical Methods for Robust Control System Design, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
181751
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