DocumentCode :
307269
Title :
Synthesis of optimal H controllers via LQG-based loop shaping design
Author :
Yang, Ciann-Dong ; Chang, Chia-Yuan ; Sun, Yun-Ping
Author_Institution :
Inst. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan, Taiwan
Volume :
1
fYear :
1996
fDate :
11-13 Dec 1996
Firstpage :
739
Abstract :
Synthesis of optimal H controllers is formulated as a loop-shaping problem where the desired closed-loop shape to be pursued is a flat frequency response of the largest singular value. The weighted H2 optimization technique used in LQG/LTR is exploited in the loop shaping procedures to generate a sequence of H2 controllers converging to the optimal H controller. The resulting optimal H controller not only has the inherent robust property due to H criterion but also possesses the nice H2 control structure, being easy to compute and implement. A flight control example is demonstrated to show that the numerical accuracy of the present LQG-based H synthesis is comparable to the conventional H approach, i.e. γ-iteration
Keywords :
H control; aircraft control; control system synthesis; frequency response; linear quadratic Gaussian control; military aircraft; optimisation; robust control; transfer function matrices; γ-iteration; H criterion; H2 controllers; LQG-based loop shaping design; LQG/LTR; closed-loop shape; flat frequency response; flight control; numerical accuracy; optimal H controllers; weighted H2 optimization technique; Aerospace control; Control system synthesis; Control systems; Frequency response; Hydrogen; Optimal control; Robust control; Shape control; Stability criteria; Sun;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
ISSN :
0191-2216
Print_ISBN :
0-7803-3590-2
Type :
conf
DOI :
10.1109/CDC.1996.574441
Filename :
574441
Link To Document :
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