Title :
Decomposed Fliess functional expansion and its application to attitude control of missiles
Author :
Cheng, Daizhan ; Qiao, Yupeng ; Yuan, Yanyan
Author_Institution :
Key Lab. of Syst. & Control, Chinese Acad. of Sci., Beijing, China
Abstract :
This paper investigates the Fliess functional expansion of input-output decomposable systems. It is proved that under suitable state feedback the closed-loop system has a Fliess functional expansion of finite terms. This form has two advantages: (1) providing a precise input-output mapping; (2) tremendously reducing the complexity of computation and making the online control design available. It is proved that the model of attitude control of missiles satisfies this decomposable requirement. Hence, the finite Fliess functional expansion technique is applicable to it. Detailed algorithm is provided for the design of attitute control.
Keywords :
attitude control; closed loop systems; computational complexity; control system synthesis; missile control; state feedback; attitude control; closed-loop system; computational complexity; finite Fliess functional expansion technique; input-output decomposable systems; input-output mapping; missiles; online control design; state feedback; Aerospace control; Aircraft; Algorithm design and analysis; Control design; Control systems; Error correction; Intelligent actuators; Missiles; Nonlinear systems; State feedback; Fliess functional expansion; Nonlinear system; attitude control; input-output decoupling; tracking;
Conference_Titel :
ICCAS-SICE, 2009
Conference_Location :
Fukuoka
Print_ISBN :
978-4-907764-34-0
Electronic_ISBN :
978-4-907764-33-3
