Title :
Adaptive sliding mode control for missile guidance law
Author :
Xiangyang Wu ; Shihua Bi ; Zheng Zhu ; Weinan Wu
Author_Institution :
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
Abstract :
The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
Keywords :
adaptive control; control system synthesis; missile guidance; variable structure systems; adaptive scheme; adaptive sliding mode control; control design; missile guidance law; missile interception problem; target acceleration; Acceleration; Adaptive systems; Closed loop systems; Estimation; Missiles; Sliding mode control; Trajectory; Adaptive control; Guidance law; Sliding mode control;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896757
