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
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;
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
DOI :
10.1109/IECON.1996.570585
