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飞行器比例导引综述
引用本文:吴文海,曲建岭,王存仁,罗德林.飞行器比例导引综述[J].飞行力学,2004,22(2):1-5.
作者姓名:吴文海  曲建岭  王存仁  罗德林
作者单位:1. 海军航空工程学院,青岛分院,山东,青岛,266041;南京航空航天大学,自动化学院,江苏,南京,210016
2. 海军航空工程学院,青岛分院,山东,青岛,266041
3. 南京航空航天大学,自动化学院,江苏,南京,210016
摘    要:基于导弹制导和机器人控制等领域,对追踪/截获动目标——导引问题的研究,综观几十年来大量国内外研究成果,系统分析与比较了各种比例导引律的含义、特点与性能。指出纯比例导引及其改进是非常有效的导引方式,可以有效地用于机动目标追踪/截获导引,能为相关领域机动目标导引问题的研究,包括战斗机追踪导引设计提供参考。

关 键 词:导引律  追踪  飞行器  目标
文章编号:1002-0853(2004)02-0001-05
修稿时间:2003年5月6日

An Overview of the Proportional Navigation
WU Wen-hai.An Overview of the Proportional Navigation[J].Flight Dynamics,2004,22(2):1-5.
Authors:WU Wen-hai
Institution:WU Wen-hai~
Abstract:Based on the large amount of study on missile navigation-interception laws and robot control, this paper gives an outline of study results of various proportional navigation laws and addresses the definitions, performances and characteristics of the main type of proportional navigation laws. It is mainly point out, by comparative analysis, that the pure proportional navigation,including it's various improved modes, is the most effective navigation-interception law,which can be effectively used to pursuit or intercept the maneuvering targets. It is expected that this survey paper will help readers realize that PPN is the more practical and effective way than GPN and much more attention should be paid on it such as studies on PPN in other fields, including the design of pursuit-attacking guidance systems of a modern fighter.
Keywords:navigation law  pursuit  flight vehicle  target
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