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飞行器导引律综述
引用本文:罗德林,卢同心,吴顺祥.飞行器导引律综述[J].系统仿真学报,2010,22(Z1).
作者姓名:罗德林  卢同心  吴顺祥
作者单位:厦门大学,信息科学与技术学院,自动化系,厦门,361005
基金项目:航空科学基金项目(20080768004)
摘    要:对飞行器追踪拦截导引律方法、特点及其发展进行了研究与总结,包括比例导引律、最优导引律、微分对策导引律以及基于现代控制理论设计的导引律,可为今后飞行器导引律的改进和设计提供参考。

关 键 词:飞行器制导  导引律  综述  拦截  追踪  

A Survey on Guidance Laws for Flight Vehicle
LUO De-lin,LU Tong-xin,WU Shun-xiang.A Survey on Guidance Laws for Flight Vehicle[J].Journal of System Simulation,2010,22(Z1).
Authors:LUO De-lin  LU Tong-xin  WU Shun-xiang
Abstract:Study and summary are made on the guidance law methods and their characteristics, applications and development for flight vehicle pursuit and interception. The discussed guidance laws include Proportional Guidance Law, Deferential Game Guidance Law, Optimal Guidance Law and Modern Control Theory based Guidance Law. The work of this paper is expected o provide reference for the improvement and design of guidance law for the flight vehicles in the future.
Keywords:flight vehicle guidance  guidance law  survey  interception  pursuit  
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