DocumentCode :
1134149
Title :
Sensitivity Reduction by Double Perfect Model Following
Author :
Okada, Tsuyoshi ; Kihara, Masahiko ; Motoyama, Kiyohumi
Author_Institution :
National Defense Academy, Japan
Issue :
1
fYear :
1982
Firstpage :
29
Lastpage :
38
Abstract :
We propose a double perfect model following (DPMF) system which uses two models: one is used to define the desirable response and the other is used to reduce sensitivity to parameter perturbation. The concept is shown and methods of model selection and controller synthesis are discussed, followed by numerical examples and an aircraft control example which demonstrate performance of the DPMF concept. It is shown that the DPMF system can be less sensitive than a nominally equivalent single perfect model following (SPMF) system and that sensitivity reduction is enhanced by proper selection of the model. It is also shown that the sensitivity of multiinput systems can be reduced componentwise or blockwise by using a decoupled type model.
Keywords :
Aerodynamics; Aerospace control; Aerospace engineering; Aircraft; Control system synthesis; Control systems; Eigenvalues and eigenfunctions; Mathematical model; Optimal control; Rockets;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1982.309203
Filename :
4102615
Link To Document :
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