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反舰导弹末端机动的突防效果研究
引用本文:顾文锦,赵红超,王凤莲.反舰导弹末端机动的突防效果研究[J].宇航学报,2005,26(6):758-761.
作者姓名:顾文锦  赵红超  王凤莲
作者单位:1. 海军航空工程学院控制工程系,烟台,264001
2. 海军后勤技术装备研究所,北京,100074
摘    要:利用共轭系统和拉氏变换技术,重点研究了反舰导弹的螺旋机动和摆式机动的突防效果。螺旋机动和摆式机动的加速度可以用纵向和航向平面内的加速度分量来表示。在平面内分析机动加速度引起的稳态脱靶量得到了简单的脱靶量解析解。利用该解析解,分析了机动持续时间对稳态脱靶量的影响。将纵向和航向平面内的稳态脱靶量综合起来得到了螺旋机动或者摆式机动所引起的稳态脱靶量。仿真结果表明这两种非平面机动方式比平面机动方式具有更好的突防效果。

关 键 词:反舰导弹  末端机动  突防  共轭系统  脱靶量
文章编号:1000-1328(2005)06-0758-04
收稿时间:11 24 2004 12:00AM
修稿时间:2004-11-242005-05-01

Reasearch on the Penetration Effect of Terminal Maneuver for Anti-ship Missiles
GU Wen-jin,ZHAO Hong-chao,WANG Feng-lian.Reasearch on the Penetration Effect of Terminal Maneuver for Anti-ship Missiles[J].Journal of Astronautics,2005,26(6):758-761.
Authors:GU Wen-jin  ZHAO Hong-chao  WANG Feng-lian
Institution:1. Department of Control Engineering, Naval Aeronautical Engineering Institute, Yantai 264001; 2. Naval Logistic Technology and Equipment Research Institute, Beijing 100074, China
Abstract:The penetration effect of spiral maneuver and cycloid maneuver has been mainly researched for antiship missiles using the adjoint system and Laplace transform technique.The accelerations of spiral maneuver and cycloid maneuver can be expressed by their components in the pitch plane and the yaw plane.The simple solution of the miss distance has been obtained by analyzing the steadystate miss distance resulted from the maneuver acceleration in the plane.The effect of the maneuver continuing time on the steadystate miss distance is researched using the above solution.Synthesizing the steadystate miss distances of the pitch plane and the yaw plane gives the steadystate miss distance caused by the spiral maneuver or the cycloid maneuver.The simulation results show that the two forms of nonplanar maneuvers have better penetration effect than the forms of planar maneuvers.
Keywords:Anti-ship missile  Terminal maneuver  Penetration  Adjoint system  Miss distance
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