DocumentCode :
274713
Title :
Weighting function specification in H design [military helicopter]
Author :
Kellett, M.G. ; White, B.A.
Author_Institution :
R. Mil. Coll. of Sci., Shrivenham, UK
fYear :
1991
fDate :
25-28 Mar 1991
Firstpage :
1035
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 given some indication of 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 should 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; closed loop systems; control system synthesis; helicopters; military systems; optimal control; stability; H design; actuator movement monitoring; battlefield helicopter; channel bandwidths; closed loop system; cost function weights; rate feedback channel weights; sensitivity function weights; time responses; weighting function specification;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Control 1991. Control '91., International Conference on
Conference_Location :
Edinburgh
Print_ISBN :
0-85296-509-5
Type :
conf
Filename :
98593
Link To Document :
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