DocumentCode
2402527
Title
Quantitative robust optimal control system design and flight control application
Author
Lin, Chih-Min ; Ying, Chen-Ling
Author_Institution
Dept. of Electr. Eng., Yuan-Ze Inst. of Technol., Chungli, Taiwan
Volume
3
fYear
1996
fDate
5-10 Aug 1996
Firstpage
1382
Abstract
The design method of a quantitative robust optimal control system is developed. Wiener-Hopf linear quadratic optimal control and quantitative feedback theory are applied to achieve the optimal system control. In this design, two frequency-dependent weighting functions are shaped and two-degree-of-freedom compensators are designed to achieve the robust optimal control
Keywords
aerospace control; compensation; feedback; linear quadratic control; optimal control; robust control; Wiener-Hopf linear quadratic optimal control; flight control application; frequency-dependent weighting functions; quantitative feedback theory; quantitative robust optimal control system; two-degree-of-freedom compensators; Aerospace control; Algorithm design and analysis; Control systems; Design methodology; Feedback; Frequency; Optimal control; Robust control; Robustness; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics, Control, and Instrumentation, 1996., Proceedings of the 1996 IEEE IECON 22nd International Conference on
Conference_Location
Taipei
Print_ISBN
0-7803-2775-6
Type
conf
DOI
10.1109/IECON.1996.570585
Filename
570585
Link To Document