DocumentCode :
2915335
Title :
Sliding mode control based guidance law with impact time constraints
Author :
Kumar, S.R. ; Ghose, Debasish
Author_Institution :
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
fYear :
2013
fDate :
17-19 June 2013
Firstpage :
5760
Lastpage :
5765
Abstract :
In this paper, the sliding mode control based guidance laws to intercept stationary targets at a desired impact time are proposed. Then, it is extended to constant velocity targets using the notion of predicted interception. The desired impact time is achieved by selecting the interceptor´s lateral acceleration to enforce a sliding mode on a switching surface designed using non-linear engagement dynamics. Numerical simulation results are presented to validate the proposed guidance law for different initial engagement geometries, impact times and salvo attack scenarios.
Keywords :
acceleration control; control system synthesis; missile guidance; nonlinear control systems; variable structure systems; velocity control; constant velocity target; impact time constraint; initial engagement geometries; lateral acceleration; nonlinear engagement dynamics; predicted interception; salvo attack scenario; sliding mode control based guidance law; switching surface; Geometry; Navigation; Sliding mode control; Switches; Time factors; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2013
Conference_Location :
Washington, DC
ISSN :
0743-1619
Print_ISBN :
978-1-4799-0177-7
Type :
conf
DOI :
10.1109/ACC.2013.6580740
Filename :
6580740
Link To Document :
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