Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Journal of Beijing Institute of Technology》 1991-03
Add to Favorite Get Latest Update

On the Pursuit- Evasion Strategy Between Anti -Tank Missiles and Tanks

Wu Xinsheng Wen Zhonghui (Department of Flight Vehicle Engineering)  
In order to improve the ability of adaptation of anti-tank missiles in various gaming circumstances , a new concept employing the theory of differential games to the design of missile controls is presented . A missile - target differential game model is established and numerically solved . Various factors such as the introduction of maneuvering of the target and changes in aerodynamic forces on the missiles etc , aifecting the flight - control loop design, is discussed . As conventional feedback control can only adapt to a single condition of flight being thus unable to meet the multiplicity of missile control response characteristics in recurring in the course of flight , this proposal provides a way out, capable of suggesting useful data in intelligent control of missiles .
【CateGory Index】: TJ 761.12 ; TJ 765
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
Chinese Journal Full-text Database 10 Hits
1 Tuo Huaide(Shaanxi Qinghua Electro-Mechanical Research Institute,Changan,Shaanxi,710111);MATRIX METHOD IN THE DERIVATION OF FORMULAS AMONG ANGLES OF ROTATION IN ROTATORS HAVING 3 DEGREES OF FREEDOM[J];Acta Armamentarii;1996-02
2 Yu Yingjie Zhang Yun Liu Zaozhen (Department of Mechatronic Engineering, Beijing Institute of Technology, Beijing, 100081);COORDINATE SYSTEMS FOR USE ON GUIDED BOMB'S DYNAMICS OF FLIGHT[J];Acta Armamentarii;2002-02
3 Qi Zhanyuan (Beijing Institute of Technology, Beijing, 100081) Xu Wenxu Zhang Gengyu (Unit 63961, PLA);A STUDY ON THE METHOD OF JUDGEMENT FOR TARGET HITTING IN SHOOTING EMULATION[J];Acta Armamentarii;2003-01
4 ZHANG Cheng, YANG Shu-xing(School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China);Study on Range Correction of Attitude Stabilized Rocket[J];Acta Armamentarii;2005-02
5 SONG Zhen-duo, DIAO Qing, XU Wen-xu(Unit 63961,PLA, Beijing 100012, China);Ballistic Model and Simulation of a Portable Antitank Missile Steering to Hit on Top of the Tank at Terminal Trajectory[J];Acta Armamentarii;2005-02
6 ZHAO Hong-chao,GU Wen-jin,MA Deng-wu(Naval Aeronautical Engineering Institute,Yantai,Shandong 264001,China);Output-redefinition-based Variable Structure Control for Aerodynamic Missiles[J];Acta Armamentarii;2005-06
7 SHANG An-li~1,YU De-hai~2,GU Wen-jin~1 (1.Research Institute of Power Electric,Naval University of Engineering,Wuhan 430033,Hubei,China;2.Department of Automatic Control,Naval Aeronautical Engineering Academy,Yantai 264001,Shandong,China;3.Educational Technique Center,Naval Aeronautical Engineering Academy,Yantai 264001,Shandong,China);Missile Autopilot Design Based on Dynamic Second Order Sliding Mode Control[J];Acta Armamentarii;2006-01
8 WEI Jing-biao~1,ZHENG Hua-li~2(1.Army Aviation Research Institute,Beijing 101121,China;2.Unit 63961 PLA,Beijing 100012,China);Initial Missile Ballistic Analysis Under the Condition of the Interference of a Helicopter's Rotor Down-wash Flow[J];Acta Armamentarii;2006-06
9 ZOU Ru-ping,ZHANG Yan-feng(No.203 Research Institute of China Ordnance Industries,Xi'an 710065,Shaanxi,China);Design of Self-spin Frequency for Rotating Missiles[J];Acta Armamentarii;2007-02
10 SONG Jin-wu1,XIA Qun-li2,XU Jin-xiang2 (1.Unit 63961 of PLA,Beijing 100012,China;2.School of Mechatronic Engineering,Beijing Institute of Technology,Beijing 100081,China);Modeling and Analysis of Guidance Loop with Velocity Pursuit Guidance Law[J];Acta Armamentarii;2008-03
China Proceedings of conference Full-text Database 5 Hits
1 Sun Dong-yan Wang De-hu Pan Hong-hua Ma Lemei (Dalian Naval Academy,Liaoning,Dalian,116018);The Simulation of Guided Munition Three-points Trajectory Based on Matlab[A];[C];2008
2 Su Hao-qin Duan ya Hao zhi-guo Li hong-bo Li ping-kun (1.China Academy of Aerospace Aerodynamics,Beijing,100074);Optimal Trajectory with H_2/H_∞ Controller and Genetic Algorithm[A];[C];2008
3 Quan Weili Yao Xiaoxian Lin Fan (School of Aerospace Science and Engineering Beijing lnstitute of Technology Beijing 100081 China);Analysis on the dynamic behavior of ram-air servo system[A];[C];2008
4 Sun Xiaoxu Shan Jiayuan (School of Astronautics Beijing Institute of Technology Beijing 100081 China);Adaptive sliding Mode DI controller Designed Based on Neural Network[A];[C];2008
5 Dong Xi-Jun Fei Min (Shanghai Electro-Mechanical Engineering Institute.Shanghai.200233);Modular Design of Guide and Control Simulation Software[A];[C];2009
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved