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反舰导弹最优滑模制导律仿真研究
引用本文:冯志刚,杨希祥.反舰导弹最优滑模制导律仿真研究[J].飞行力学,2007,25(3):38-41.
作者姓名:冯志刚  杨希祥
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
基金项目:武器装备预研基金 , 武器装备预研基金 , 国防科技大学校科研和教改项目
摘    要:针对传统比例导引法攻击机动目标的不足,建立了三维空间中反舰导弹和目标的相对运动模型,在研究反舰导弹攻击非机动目标的最优制导律基础上,利用俯仰和偏航两个平面相叠加的方法,结合滑模控制理论设计了工程上易于实现的三维模型下的反舰导弹最优滑模制导律。仿真结果表明,给出的导引律在攻击机动目标时制导精度高、脱靶量小,导引控制过程具有良好的动态性,性能明显优于传统的比例导引律。

关 键 词:反舰导弹  最优制导律  最优滑模制导律
文章编号:1002-0853(2007)03-0038-04
修稿时间:2006-09-19

Simulation Research on Optimal Sliding-Mode Guidance Law for an Anti-Ship Missile
FENG Zhi-gang,YANG Xi-xiang.Simulation Research on Optimal Sliding-Mode Guidance Law for an Anti-Ship Missile[J].Flight Dynamics,2007,25(3):38-41.
Authors:FENG Zhi-gang  YANG Xi-xiang
Institution:College of Aerospace and Material Engineering, NUDT, Changsha 410073, China
Abstract:To overcome the shortages of the traditional proportional guidance in attacking maneuvering targets,the paper firstly established the relative motion models for the anti-ship missile and the target in three dimensions,then based on the optimal guidance law for aiming at non maneuvering targets and the sliding-mode control theory,the optimal sliding-mode guidance law in three dimensions,which was more easily-accomplished in engineering,was derived by making the pitch plane and yaw plane superposition.Simulation studies show that the proposed law in this paper has better guidance accuracy and better dynamic property during pursuit-control processing and it is superior to proportional navigation.
Keywords:anti-ship missile  optimal guidance law  optimal sliding-mode guidance law
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