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
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;
Conference_Titel :
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location :
Mianyang
Print_ISBN :
978-1-4244-8737-0
DOI :
10.1109/CCDC.2011.5968388
