DocumentCode
1910891
Title
Design Method of Eigenvalue Assignment based on Standard Characteristic Polynomial
Author
Li Aijun ; Xu Lina ; Wenjie, Meng ; Wang Changqing
Author_Institution
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
Volume
4
fYear
2009
fDate
10-11 Oct. 2009
Firstpage
180
Lastpage
183
Abstract
Eigenvalue assignment method based on standard characteristic polynomial is proposed in order to resolve the uncertainty of ideal eigenvalue choice in modern control theory and the difficultly in engineering implementation of modern control system design methods. Mathematical solving process of the method is given. There is only one design parameter which is easy to calculate. We can choose the parameter according to system responding time or tuning time. Control system of an aircraft was designed and simulated by using proposed method. Simulation results show that the method is capable of achieving desire control quality, and designing procedure is simple. Furthermore, robustness of the control system is good.
Keywords
aircraft control; closed loop systems; control system synthesis; eigenstructure assignment; polynomials; stability; aircraft; closed loop systems; control system design methods; control theory; design parameter; eigenvalue assignment method; ideal eigenvalue choice; mathematical solving process; robustness; standard characteristic polynomial; system responding time; tuning time; Aerospace engineering; Aircraft; Control system synthesis; Control systems; Control theory; Design engineering; Design methodology; Eigenvalues and eigenfunctions; Polynomials; Uncertainty; aircraft; closed loop system; eigenvalue assignment; standard characteristic polynomial;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computation Technology and Automation, 2009. ICICTA '09. Second International Conference on
Conference_Location
Changsha, Hunan
Print_ISBN
978-0-7695-3804-4
Type
conf
DOI
10.1109/ICICTA.2009.760
Filename
5288244
Link To Document