DocumentCode
306557
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
Volume
2
fYear
1996
fDate
11-13 Dec 1996
Firstpage
1315
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;
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.1996.572682
Filename
572682
Link To Document