DocumentCode
233861
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
fYear
2014
fDate
28-30 July 2014
Firstpage
960
Lastpage
965
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896757
Filename
6896757
Link To Document