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《JOURNAL OF ASTRONAUTICS》 1994-01
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ESTIMATION OF MISS DISTANCE AND GENERALIZED PROPORTIONAL NAVIGATION

Jiang Yuxian(Beijing University of Aeronautics and Astronautics)  
An approach for estimating the miss distance of homing missile with proportional navigation is presented.According to the approach,only the delay of a guidance system,the relative velocity of missile and target are known, the value of miss distance can be estimated. The prospect to use the generalized proportional navigation for reducing miss distance is also discussed.
【Fund】: 航空科学基金
【CateGory Index】: V448.23
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【References】
Chinese Journal Full-text Database 1 Hits
1 CHEN Huan;LIU Jiao-long;WEI Jian-li;YU Yun-feng;College of Astronautics,Northwestern Polytechnical University;System Theory and Simulation Technology Research Division,Beijing Aerospace AutomaticControl Institute;;Design of optimal guidance law with higher-order dynamic lags[J];飞行力学;2014-01
【Co-references】
Chinese Journal Full-text Database 8 Hits
1 WANG Hong-qiang1,2,SHAO Xiao-wei1,ZHOU Gang2,DUAN Deng-ping1(1.Shanghai Jiaotong University,Shanghai 200240,China; 2.Northwest Institute of Nuclear Technology,Xi'an 710024,China);A Study on Modified Combined Terminal Guidance Law[J];计算机技术与发展;2011-12
2 XU Yan-ke1,LIANG Xiao-geng1,2(1.School of Automation,Northwestern Polytechnical University,Xi'an 710072,China,2.China Airborne Missile Academy,Luoyang 471009,China);An Improved Terminal Guidance Method Insensitive to Residual Flight Time Estimation Error[J];火力与指挥控制;2011-10
3 WANG Hui1,LIN Defu1,CHENG Zhenxuan2(1 School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China; 2 China North Industries Group Corporation,Beijing 100821,China);The Research on Optimal Proportional Navigation Guidance with Single Dynamic Lag[J];弹箭与制导学报;2011-04
4 XU Tao1,YANG Jun1,ZHAN Jian-chao1,2 (1.College of astronautics,NorthWestern Polytechnical University,Xi'an Shanxi 710072,China;2.XuZhou Airforce College,Xuzhou Jiangsu 221000,China);Research on Engineering Application Method of Infrared Missile Based on Optimal Guidance[J];计算机仿真;2010-02
5 XIAO Zeng-bo, LEI Hu-min, MA Fu-zhou( AFEU ,Missile Institute, Shaanxi Sanyuan 713800, China);Research on Optimum Terminal Guidance Law[J];现代防御技术;2009-02
6 LI Yi1,SONG Zhenduo2,LIU Dezhong1(1 School of Aerospace Science and Engineering,Beijing Institute of Technology,Beijing 100081,China;2 No.63961 Unit,Beijing 100012,China);Derivation of First-order Optimal Guidance Law with Optimal Control Theory[J];弹箭与制导学报;2008-05
7 ZHANG Hong,XIA Qun-li,QI Zai-kang,RONG Jing-jing(School of Aerospace Science and Engineering,Beijing Institute of Technology,Beijing 100081,China);Augmented proportional navigationwith maneuvering target compensation[J];红外与激光工程;2007-S2
8 Jiang Yuxian(Beijing University of Aeronautics and Astronautics);ESTIMATION OF MISS DISTANCE AND GENERALIZED PROPORTIONAL NAVIGATION[J];宇航学报;1994-01
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