Title :
Two-degree-of-freedom optimal flight control system design
Author :
Lin, Chih-Min ; Wu, Jim-Min
Author_Institution :
Dept. of Electr. Eng., Yuan-Ze Inst. of Technol., Chungli, Taiwan
Abstract :
A linear quadratic optimal control system is described and applied to flight control system design. By the parametric two-degree-of-freedom controller configuration, the multivariable linear quadratic optimal system design is developed and its application to the flight control of the longitudinal motion for aircraft is also illustrated
Keywords :
aircraft control; control system synthesis; feedback; linear quadratic control; multivariable control systems; linear quadratic optimal control system; longitudinal motion; multivariable linear quadratic optimal system; two DOF optimal flight control system design; Adaptive control; Aerospace control; Aircraft; Control systems; Design methodology; Linear feedback control systems; Matrix decomposition; Motion control; Optimal control; System performance;
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
Print_ISBN :
0-7803-3590-2
DOI :
10.1109/CDC.1996.572682
