DocumentCode
2776222
Title
Attitude control of missiles via finite-terms Fliess expansion
Author
Qiao, Yupeng ; Shen, Dongbin
Author_Institution
Coll. of Autom. Sci. & Eng., South China Univ. of Technol., Guangzhou, China
fYear
2009
fDate
17-19 June 2009
Firstpage
1021
Lastpage
1026
Abstract
This paper investigates the attitude control of missiles. We use the decomposed Fliess functional expansion of input-output decomposable systems to describe the outputs. Then under piece-wise constant admissible value controls, the optimal control on finite time durations can be obtained. The method tremendously reduces the complexity of computation and makes the online control design available. The effectiveness of the proposed method is shown by numerical simulations.
Keywords
attitude control; computational complexity; missile control; nonlinear systems; computational complexity; constant admissible value controls; finite terms Fliess expansion; input-output decomposable systems; missiles attitude control; nonlinear system; Automatic control; Automation; Educational institutions; Error correction; Feedback; Intelligent actuators; Missiles; Nonlinear systems; Optimal control; Robust control; Attitude control; Finite-terms Fliess functional expansion; Input-output decoupling; Nonlinear system;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference, 2009. CCDC '09. Chinese
Conference_Location
Guilin
Print_ISBN
978-1-4244-2722-2
Electronic_ISBN
978-1-4244-2723-9
Type
conf
DOI
10.1109/CCDC.2009.5191580
Filename
5191580
Link To Document