Integrated missile guidance and control design with smooth adaptive sliding mode control

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	Integrated missile guidance and control design with smooth adaptive sliding mode control
	Zhou, Jialing ; Yang, Jianying
	2015
DOI	10.1109/ChiCC.2015.7260451
英文摘要	This paper considers the problem of a missile intercepting a maneuvering target with demand for fast finite-time convergence and anti-chattering. Based on the widely used proportional navigation strategy, a novel integrated guidance and control (IGC) scheme is proposed, which is formulated as a second-order affine nonlinear system with uncertainties. Then the smooth adaptive nonsingular terminal sliding mode control (SANTSMC) method which is proposed in our pervious work is applied to this IGC scheme. By virtue of the SANTSMC method, the uncertainties with unknown bounds can be addressed, fast finite-time convergence can be achieved, and the chattering problem can be well solved. ? 2015 Technical Committee on Control Theory, Chinese Association of Automation.; EI; 5206-5211; 2015-September
会议录	34th Chinese Control Conference, CCC 2015
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/423486]
专题	工学院
推荐引用方式 GB/T 7714	Zhou, Jialing,Yang, Jianying. Integrated missile guidance and control design with smooth adaptive sliding mode control[C]. 见:.