A program flight control method applicable for blind area

	A program flight control method applicable for blind area
	Gao F.; Tang S.-J.; Shi J.; Yang C.-L.
	2014
发表期刊	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
ISSN	ISBN/10010645
卷号	34 期号:2 页码:117-122
摘要	In order to weaken the negative influence of imaging seeker blind area on the impact performance, the effect on trajectory parameters from rudder angle was analyzed, and a control method based on rudder scheme was proposed. Based on this method, the selection principle of the rudder scheme was discussed, and four feasible variation rules were given to simulate and compare with the effect of the situation when the rudder angle was assigned as a constant in blind area. Then the better two in the four variation rules were optimal designed to achieve better effect. Results of simulations illustrate that the method can improve the hit accuracy of missiles, and decrease the angle of attack and normal overload of the impact point.
收录类别	EI
语种	中文
文献类型	期刊论文
条目标识符	http://ir.ciomp.ac.cn/handle/181722/43695
专题	中科院长春光机所知识产出
推荐引用方式 GB/T 7714	Gao F.,Tang S.-J.,Shi J.,et al. A program flight control method applicable for blind area[J]. Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology,2014,34(2):117-122.
APA	Gao F.,Tang S.-J.,Shi J.,&Yang C.-L..(2014).A program flight control method applicable for blind area.Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology,34(2),117-122.
MLA	Gao F.,et al."A program flight control method applicable for blind area".Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology 34.2(2014):117-122.

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