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超音速反舰导弹的最优末制导律研究
引用本文:赵红超,王凤莲,顾文锦.超音速反舰导弹的最优末制导律研究[J].航空兵器,2005(3):8-11.
作者姓名:赵红超  王凤莲  顾文锦
作者单位:1. 海军航空工程学院,山东烟台,264001
2. 海军后勤技术装备研究所,北京,100074
摘    要:研究了超音速反舰导弹的末制导问题。利用伪控制变量的概念,建立了简单的描述反舰导弹与目标舰艇相对运动的状态方程。根据最优控制理论,推导了反舰导弹的最优末制导律,保证脱靶量指标和能量消耗均为最小。最后,举例进行了全弹道仿真研究,仿真结果表明了所设计的最优末制导律的有效性。

关 键 词:超音速反舰导弹  最优控制  末制导律  脱靶量  能量消耗
文章编号:CN41-1228(2005)03-0008-03
修稿时间:2004年10月28

Research on Optimal Terminal Guidance Law for Surpersonic Anti-Ship Missile
ZHAO Hong-chao,Wang Feng-lian,GU Wen-jin.Research on Optimal Terminal Guidance Law for Surpersonic Anti-Ship Missile[J].Aero Weaponry,2005(3):8-11.
Authors:ZHAO Hong-chao  Wang Feng-lian  GU Wen-jin
Abstract:The problem of terminal guidance of a surpersonic anti-ship missile is studied in this paper. Using the concept of pseudo control variable, a simple state equation is constructed which describes the relative motion between an anti-ship missile and a target ship. The optimal terminal guidance law is deduced for the anti-ship missile according to the optimal control theory. It guarantees the minimum of miss amount and energy consuming. Finally, a simulation example is illustrated to research, and the results show the validity of the designed optimal terminal guidance law.
Keywords:surpersonic anti-ship missile  optimal control  terminal guidance law  miss amount  energy consuming
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