Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Tactical Missile Technology》 2014-01
Add to Favorite Get Latest Update

Design of Horizontal Flight Trajectory for Supersonic Rocket Target Based on Controlled Scheme

Zhang Yan;Shan Shizhuo;Unit 92941 Element 93;  
Considering the more defects exist in the no controlled scheme for achieving horizontal flight,a design idea about achieving the horizontal flight by assembling canard control vane and simple control system on the prototype rocket projectile is put forward,and the system concept is described. In the end, according to the aerodynamic characteristic data and missile structure data,the flight trajectory under the different condition are analyzed by using simulation calculations,and combining with the results,the concept of supplying target are analyzed. The result of trajectory simulation indicates that a more straight smooth flight trajectory could be gained by choosing the different launch angle and the control program of rudder deflection angle.
【CateGory Index】: TJ415
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 4 Hits
1 Zhang Bangchu Han Zipeng Fan Yanfei (Power Eng. College, NUST, Nanjing, 210094);DESIGN OF THE LEVEL TRAJECTORY OF CRUISE MISSILE SIMULATED TARGET[J];Journal of Ballistics;2003-02
2 LI Xiao-bin1,2,WANG Yong-jie1,SUN Xiao-feng1(1.Unit 92941 of PLA,Huludao 125000,China;2.Scientific Research Post-doctor Workstation,Unit 92493 of PLA,Huludao 125000,China);System Design of Simple Control Rocket Target[J];Journal of Ballistics;2010-01
3 Fu Jinglai,Chen Tao(Unit 91851,Huludao Liaoning 125001,China);Research on Rocket Projectile Trajectory Improvement Based on Vertical Attack Way[J];Tactical Missile Technology;2011-01
4 Liang Ming(Unit 91851,Huludao Liaoning 125001,China);Dynamic Model Parameter Identification and Trajectory Simulation of Target Missile[J];Tactical Missile Technology;2012-03
Chinese Journal Full-text Database 10 Hits
1 XIE Jian-hua2, MA Li-yuan1, ZHANG Rui2 (1. College of Science, Nanjing University of Science and Engineering, Nanjing 210094, China; 2. Dept. of Missile Engineering, Ordnance Engineering College, Shijiazhuang 050003, China);Control of Virtual Arm of Missile Virtual Operation System[J];Ordnance Industry Automation;2004-05
2 PAN Qing-jun1,2,HUANG Zao-wen1, YANG Xing-chao2 (1. Material Institute, Huazhong University of Science & Technology, Wuhan 430074, China; 2. Aeronautical Repair Engineering Department, First Aeronautical Institute of Air Force, Xinyang 464000, China);Damage Calculation and Simulation of the Discrete Rod Warhead to an Aircraft[J];Ordnance Industry Automation;2006-08
3 TONG Yong, XIAO Hui-xin, QU Hong-xing, XIAO Qi (Administrant Brigade of Graduate, Air Defense Forces Command Academy Zhengzhou 450052, China);Analyze on Field Training System Simulation for Portable Anti-Aircraft Missile[J];Ordnance Industry Automation;2007-02
4 PU Yuan1,2,WANG Wu1,LIU Li-wu1 (1. Institute of Command & Technology of Equipment,Beijing 101416,China; 2. Xichang Satellite Launch Center,Xichang 615000,China);Analysis of Rotational Speed Influence on Controllable Trajectory of Guided Projectile at Low Roll Rate[J];Ordnance Industry Automation;2009-11
5 Peng Shaoxiong,Li Xueyuan,Yuan Hongwu,Zou Qiang(Dept.of Aircraft Engineering,Naval Aeronautical & Astronautical University,Yantai 264001,China);Study on Hand-Over Error Model of Dual Combined Guidance Ship-to-Air Missile[J];Ordnance Industry Automation;2012-02
6 CHEN Wei-dong~1,LIU Xu-hua~2,SUN Yi~3(1.Department of Aerospace Engineering,Harbin Engineering University,Harbin 150001,Heilongjiang,China;2.China Flight Test Establishment,Xi'an 710089,Shaanxi,China;3.Changsha China Construction Architectural Design Institute,Changsha 410004,Hunan,China);A Research on Data Processing Method for Multiple Sets of Data from the Same Test[J];Acta Armamentarii;2007-01
7 HUO Peng-fei(1,2),SHI Kun-lin1,YUAN Wei-zheng2 (1.Xi'an Institute of Electromechnical Information Technology,Xi'an 710065,Shaanxi,China;2.School of Mechatronics Engineering,Northwestern Polytechnical University,Xi'an 710072,Shaanxi,China);Research on Trajectory Controlled Optimization for Trajectory Correction Fuze Using Maximum Principle[J];Acta Armamentarii;2007-03
8 SHEN Yan-hang,ZHOU Zhou(School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,Shaanxi,China);A Method of Cooperative Engagement Control for Attack Uninhabited Air Vehicles[J];Acta Armamentarii;2008-10
9 GUI Qiu-yang,QIU Zhi-ming (Naval Armament Academy,Beijing 100161,China);Model of the Estimation of Fire Intersection Based on Vertical Launch Weapons[J];Acta Armamentarii;2008-11
10 LI Chen-ming1,HAN Zi-peng2,LIU Yi-xin1,GU Jian-ping3(1.Nanjing Artillery Academy of PLA,Nanjing 211132,Jiangsu,China;2.School of Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China;3.School of Material Engineering,Nanjing Institute of Technology,Nanjing 211167,Jiangsu,China);Study on Stable Scanning of Terminal Sensing Ammunition Based on Quaternion Amendment[J];Acta Armamentarii;2009-04
China Proceedings of conference Full-text Database 10 Hits
1 Cheng Wei Zhang Zhi-hu Qian Ji-cheng Jia Hong-guang (Army Aviation Institute,Beijing,101123);Simulation of Video Guided Seeker[A];[C];2008
2 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
3 Tang Jiang~1 Xie Xiao-fang~1 Liu Ji-wei~2 Huang Quan-xin~1 (1.Department of Weapon Science and Technology in Naval Aeronautical Engineering University,Shandong,Yantai,264001)(2.DOE of PLA Navy,Beijing,100000);Research on Remote Control Simulation System for the “Man-in-the-Loop” Missile[A];[C];2008
4 Cheng Wei~1 Zhang Zhi-hu~1 Wang Hong-yu~1 Hua Yong~2 Wang Xu-dong~1 (1.Army aviation Institute,Beijing,101123;2.Unit61902,Sichuan,644000);Research on Getting the Position of a Object on Multi-function Colour Display for Air Training Simulation[A];[C];2010
5 Zhen LIU,Tao ZHANG Department of Automation,Tsinghua University,Beijing,China;Design and Simulation of PID-Based Missile Stability Control Loop[A];[C];2011
6 Song Xiaodong Yao Xiaoxian Yu Zhiyuan (School of Aerospace of Science and Engineering Beijing Institute of Technology Beijing 100081 China);study of pressure control of intelligent pumping source based on Fuzzy-SMC[A];[C];2008
7 Wang Na Xi Jianhui Huang Yu Zhao Wencheng (School of Automation Shenyang Institute of Aeronautical Engineering Shenyang 110136 China);Analysis on Dutch Roll Modal of Unmanned Aerial Vehicle with the Limited Deadlocking of Single Aileron[A];[C];2009
8 Tong Huijun Jia Qiumi Ji Yiguo (Ordnance Engineering Department,Aviation University of Airforce,Changchun 130022,China);Design of Simulation Experiment Platform for TV Guiding Missile Trajectory[A];[C];2008
9 ZHANG Wen-pan1, WANG Chang-ping2, GUO Zheng-hong1, LI Bo1, WU Jun-hui1 (1.Unit 63892, PLA, Luoyang 471003, China; 2.The Military Representative in 298 Corporation, Kunming 650114, China);Analysis on simulated and tested system of countermeasure against laser guided weapon[A];[C];2006
10 GAO Zhi-jie~1 WANG Shi-cheng~2 SHI Guo-hua~1 (1.The Second Artillery Armament Academy,Beijing 100085,China;2.The Second Artillery Engineering College,Xi'an 710025,China);Hardware in-the-loop simulation of aerodynamically stabilized laser-guided aerial bomb[A];[C];2007
【Secondary Citations】
Chinese Journal Full-text Database 4 Hits
1 Wang Hao (Nanjing University of Science and Technology, Nanjing, 210094);A MODEL FOR THE FIRING PROCESS OF THE INTERNAL-COMBUSTION GASBAG SUBMUNITION AND ITS SIMULATION[J];Acta Armamentarii;2001-02
2 Xue Xiaozhong ①Wei Jingbiao ①Mi Zhihao ①Shi Lixin ②Sheng Jianping ②Pan Yongping ②(①Power. College, NUST, Nanjing, 210094 ②Institute of aerborming, Nanjing, 210037)$$$$;STABLE PRICIPLE OF PNEUMATIC GYRO-RUDDER AND REUSE OF RETIRED GYROSCOPE[J];Journal of Ballistics;2001-04
3 Zhang Bangchu Han Zipeng Fan Yanfei (Power Eng. College, NUST, Nanjing, 210094);DESIGN OF THE LEVEL TRAJECTORY OF CRUISE MISSILE SIMULATED TARGET[J];Journal of Ballistics;2003-02
4 Liu Guang,Lv Jianxin(Shanghai Electro-Mechanical Engineering Institute,Shanghai 200233,China);Dynamics Simulation of Rifle Launching of Certain Missile by Means of Virtual Prototype Technology[J];Tactical Missile Technology;2005-05
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved