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《Journal of Beijing University of Aeronautics and Astronautics》 2008-02
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Trajectory optimization design for surface-to-air missile using multilayer approach

Jiang Huan Zhou Hao Chen Wanchun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)Yang Baokui(The Third Academy,China Aerospace Science and Industry Corporation,Beijing 100074,China)  
A multilayer approach to the midcourse trajectory design for a surface-to-air missile to maximize the kill probability was presented.Three layers were discussed.The first layer represented the midcourse trajectory of the missile,the second layer represented the terminal homing phase,and the third layer was the warhead damaging process.The first-layer trajectory was optimized with a constraint on the value of pitch angle at the handover point to the terminal phase.The pitch angle was used as the global parameter to combine the first and second layer in generating a field of optimum first-layer midcourse trajectories.The second-layer was a Monte-Carlo terminal homing simulation to get the average and standard deviation of miss distance,which combined the second-layer and the third-layer.The third-layer calculated the missile's kill probability by using the standard deviation of miss distance.The pitch angle and midcourse which maximizing the kill probability were the optimum results of the system.The multilayer approach demonstrates the connection between the midcourse trajectory design and the kill probability.It allows the kill probability be a measure in the midcourse trajectory optimization.Two cases that intercepting high-attitude-high-speed and low-attitude-low-speed cruising target are presented.
【CateGory Index】: TJ761.13
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【References】
Chinese Journal Full-text Database 3 Hits
1 Liu Hengjun(School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Jiang Huan Chen Wanchun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill[J];Journal of Beijing University of Aeronautics and Astronautics;2010-02
2 HU Yun-an,ZHAO Yong-tao(Department of Control Engineering,Naval Aeronautic Engineering Institute,Yantai 264001,China);Design of Guidance Law for Beyond-visual-range Interception of Ship-Air Missile and Instruction Solution[J];Journal of Ballistics;2011-01
3 CHENG Jie,GAO Wei(Depatment of Ordnance,Naval Scholar Official School,Bengbu 233012,China);Modeling and Simulation for Antiaircraft Firing Ability of Certain Type Small-Bore Warship Cannon[J];Journal of Ballistics;2011-03
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 JING Shujie ZhANG Zhirong(Henan Polytechnie University,Jiaozuo 454010,China);The New Conjugate Gradient Method with Generalized Wolfe Step Size Rule[J];Journal of Anyang Institute of Technology;2007-06
2 DU Jianguo,LI Wanhua,HE Yongsheng,LV Xueli(The Third Engineer Scientific Research Institute of the Headquarters of the General Staff,Luoyang 471023,China);Dynamic performance and mechanical model of the single pole MRD without accumulator[J];Ordnance Material Science and Engineering;2011-05
3 LIU Yun-hui,LUO Si-wei,LI Ai-jun,YU Han-bin (School of Computer and Information Technology, Beijing Jiaotong University, Beijing 100044,China);Research of Neural Network Learning Based on the View of Convex Programming[J];Journal of Northern Jiaotong University;2004-05
4 XU Hong~1,MA Jian-jun~2,LONG Jian-cheng~1,YANG Hao~1,LONG Zhao~1(1.School of Traffic and Transportation,Beijing Jiaotong University,Beijing 100044,China;2.Administration Office of Information Technology of MOR,Beijing 100844,China);Study on Model and Method of Train Working Diagram of Urban Rail Transit[J];Journal of Beijing Jiaotong University;2006-03
5 Qian Jin (Zhenjiang Watercraft College of PLA Zhenjiang 212003);Calculation Model about Availability of Multi-state Coherent System[J];Office Informatization;2009-12
6 FENG Ming-qin1, SUN Zheng-shun2 (1. Dept. of Electrical & Information Engineering, Panzhihua University, Panzhihua 617000, China; 2. Dept. of Automation, Tsinghua University, Beijing 100084, China);Modeling and Stable State Optimal Control for FCC Process[J];Ordnace Industry Automation;2002-04
7 YOU Zhi-feng, ZHAO Shu-wen, LI Yong (Brigade of Graduate, Air Defense Forces Command Academy, Zhengzhou 450052, China);Reliability-Assignment Optimization Model of Surface-to-Air Missile System with Fuzzy Targets[J];Ordnance Industry Automation;2005-03
8 WU Wen-jun1,2, PENG Xiao-long1, WANG Hui-yong1 (1. Brigade of graduate, Air Defense Forces Command Academy, Zhengzhou 450052, China; 2. NO. 71315 Army, Chinese People’s Liberation Army, Zhengzhou 450052, China);Fuzzy Fluster Analysis of Ex-Service Ship-based Weapons[J];Ordnance Industry Automation;2005-04
9 LIN Chong-yang, JIANG Qing-xiang, CHEN Jian-hu (Administrant Brigade of Graduate, Air Defense Forces Command Academy Zhengzhou 450052, China);Certain Missile Efficiency Evaluation Based on Blur Administrative Levels Analysis Method[J];Ordnance Industry Automation;2006-12
10 Zhang Jinchun1,Jin Zhe2,Wang Feng3,Li Rihua1(1.Institute of Systems Science & Mathematics,Dept.of Basic Theory,Naval Aeronautical & Astronautical University, Yantai 264001,China;2.Dept.of Scientific & Research,Naval Aeronautical & Astronautical University,Yantai 264001,China;3.No.4 Brigade of Postgraduate,Naval Aeronautical & Astronautical University,Yantai 264001,China);Study on Efficiency of Missile Weapon System Based on Extension Analysis and Transformation[J];Ordnance Industry Automation;2011-09
China Proceedings of conference Full-text Database 10 Hits
1 Liu Kun,Lin Leke,Kang Shifeng,Zhao Zhenwei,Zhu Qinglin,Chen Xiangming,Li Jianru National Key Laboratory of Electromagnetic Environment,China Research Institute of Radiowave Propagation;The Application of Singular Ground-based GNSS Receiver in the Refraction Correction of Radiowave Environment[A];[C];2012
2 Liu Yuandong Yin Yihui Yu Shaorong (Institute of Structural Mechanics,China Academy of Engineering Physics,Mianyang,Sichuan 621900 China);Structural Optimization of A Bolt-Flange Structure Based on Response Surface Design Method[A];[C];2009
3 Feng Wu,Chenyang Yang,Yafei Tian and Shiyi Mao (School of Electronics Engineering,Beihang University,Beijing 100083 China);Iterative Algorithms For LCMP Auxiliary-Vector Filter[A];[C];2003
4 YUAN Wei,SHI Gong-tao,JIANG Yong-mei (School of Electronic Science and Engineering,National University of Defense Technology,Hunan Changsha,410073;);A SAR image registration technique based on ROEWA operator and GA-Powell algorithm[A];[C];2009
5 LIU Fu-ping,YANG Chang-chun (Institute of Geology and Geophysics,Chinese Academy of Sciences,Beijing 100101,China);Numerical Calculation of Sensitivity Coefficients to the Porosity[A];[C];2003
6 Yin Chun,Wang Zhiquan,Dai Yuewei (School of Automation,Nanjing University of Science and Technology,Nanjing,210094);ON CONTROL OF OPPORTUNITY AWAITING TIME OPTIMIZATION WITH CONTRAINT ON CONTROLLER GAIN[A];[C];2009
7 Zhou Yuan Cao Zhi-xin (Navy Arms-Command Academy,Guangdong,Guangzhou,510430);Evaluating on Influenced Factor Anti-missile Efficacy of Ship-to-air Missile[A];[C];2008
8 ;A New Algorithm to Solve Linear Programming Problems with Coupled Multi-Blocks[A];[C];2005
9 Sun Yuhua Department of Mathematics and Mechanics, USTB,Beijing,100083,China;Sensitivity analysis under perturbations of both objective function coefficient and constrained matrix[A];[C];2010
10 Cai Yuan-li Zhi Qiang Lu Cang-hai (School of Electronic & Information Engineering,Xi'an Jiaotong University,Shanxi,Xi'an,710049);On the Evaluation of Operation Effectiveness for PAC-3 Anti-TBM System[A];[C];2009
【Co-references】
Chinese Journal Full-text Database 5 Hits
1 SHI Jin-guang1,XU Ming-you1,WANG Zhong-yuan1,ZHANG Bing-ling2(1.School of Power Engineering,NUST,Nanjing 210094,China;2.Ammunition Martial Representative Office of Navy Stayed Shenyang,Shenyang 110045,China);Application of Kalman Filtering in Calculation of Trajectory Falling Point of Trajectory Correction Projectiles[J];Journal of Ballistics;2008-03
2 ZHANG Feiyu,QI Zaikang(School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China);Proportional Navigation System with Noise Simplification Study[J];Journal of Projectiles,Rockets,Missiles and Guidance;2010-02
3 HU Yun-an1,ZHAO Yong-tao1,LIN Jia-xin2(1.Department of Control Engineering,Naval Aeronautical Engineering Institute,Yantai 264001,China;2.Department of Training,Naval Aeronautical Engineering Institute,Yantai 264001,China);Design of the guidance law based on the virtual target for ship-to-air missile beyond visual range[J];Flight Dynamics;2010-03
4 Zhang Youan,Ma Peibei(Department of Control Engineering,Naval Aeronautical and Astronautical University,Yantai 264001,China);Three-dimensional Guidance Law with Impact Angle and Impact Time Constraints[J];Acta Aeronautica Et Astronautica Sinica;2008-04
5 XIA Qun-li,LIU Yi-ying,QI Zai-kang,GUO Tao(School of Aerospace Science and Engineering,Beijing Inst.of Technology,Beijing 100081,China);Study of proportional navigation guidance error caused by angular noise and glint effect[J];Systems Engineering and Electronics;2008-08
【Secondary References】
Chinese Journal Full-text Database 2 Hits
1 ZHANG Longjie,XIE Xiaofang,SUN Tao,WANG Chengcheng(Department of Ordnance Science and Technology,Naval Aeronautical and Astronautical University,Yantai 264001,China);Intercept analysis of shipborne CIWS to supersonic missiles on a shortcut flight course[J];Journal of Harbin Engineering University;2013-01
2 ZHAO Yong-tao 1,2,QIU Jun 2,HU Yun-an 1(1.Department of Control Engineering,NAAU,Yantai Shandong 264001,China;2.The 92060 th Unit of PLA,Dalian Liaoning 116000,China);Design of An Optimal Midcourse Guidance Law for the Guidance Handover of the Ship-to-Air Missile[J];Journal of Naval Aeronautical and Astronautical University;2013-03
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