DocumentCode
2514935
Title
Fault tolerant control for missile guidance laws with finite-time convergence
Author
Zhu, Zheng ; Xia, Yuanqing ; Fu, Mengyin ; Wang, Shuo
Author_Institution
Dept. of Autom. Control, Beijing Inst. of Technol., Beijing, China
fYear
2011
fDate
23-25 May 2011
Firstpage
1288
Lastpage
1293
Abstract
This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault-tolerant control schemes with sliding mode control and finite-time control are proposed for the design of guidance laws to achieve the interception in the presence of bounded target acceleration. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
Keywords
missile guidance; variable structure systems; actuator fault; bounded target acceleration; fault tolerant control; finite-time control; finite-time convergence; hit-to-kill guidance law; missile guidance law; missile interception; sliding mode control; Acceleration; Actuators; Additives; Convergence; Fault tolerance; Missiles; Trajectory; Fault tolerant control; Finite-time control; Guidance law; Sliding mode control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location
Mianyang
Print_ISBN
978-1-4244-8737-0
Type
conf
DOI
10.1109/CCDC.2011.5968388
Filename
5968388
Link To Document