DocumentCode :
3664914
Title :
A continuous second-order sliding mode guidance against highly maneuverable targets
Author :
Wang Yongkun;Liu Zhongxin;Sun Mingwei;Chen Zengqiang
Author_Institution :
Department of Automation, Nankai University, Tianjin 300071, China
fYear :
2015
fDate :
7/1/2015 12:00:00 AM
Firstpage :
788
Lastpage :
793
Abstract :
Conventional proportional navigation or augmented proportional navigation guidance laws are widely used for intercepting maneuverable targets; however, they are effective only in intercepting a target with a constant velocity or a known acceleration. In this paper, a continuous second-order sliding mode guidance law is designed to intercept a highly maneuverable target in connection with the super-twisting algorithm. Meanwhile, the target maneuver information, regarded as unpredictable disturbance, is coped with by an extended state observer (ESO) and then is compensated in the guidance law. In the proposed guidance scheme, no information about target motion is needed. The closed-loop error can be guaranteed to be bounded by using Lyapunov method. The simulation results demonstrate the effectiveness and robustness of the proposed guidance method against a highly maneuverable target.
Keywords :
"Missiles","Observers","Acceleration","Heuristic algorithms","Navigation","Algorithm design and analysis","Aerodynamics"
Publisher :
ieee
Conference_Titel :
Society of Instrument and Control Engineers of Japan (SICE), 2015 54th Annual Conference of the
Type :
conf
DOI :
10.1109/SICE.2015.7285346
Filename :
7285346
Link To Document :
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