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《Journal of Sichuan Ordnance》 2013-11
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A Study on Optimizing Design of Trajectory for Glide Extended-Range Projectile

CAO Hong-jin;GE Zhi-lei;No.59 Institute of China Ordnance Industry;Northwestern Polytechnical University;  
An optimizing design of sliding extended-range is researched. The gliding extended range projectile model is established. The whole ballistic include ballistic period and sliding period. Different methods are used to optimize paragraphs ballistic. The whole ballistic achieves the optimal. Taking someone glide extended-range projectile as study object,the design of trajectory is achieved maximum extendedrange. The conclusion of this study is conducive to the design of gliding extended-range projectiles in future.
【CateGory Index】: TJ012.3
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【Citations】
Chinese Journal Full-text Database 4 Hits
1 SHI Jin-guang~1,WANG Zhong-yuan~1,YI Wen-jun~1,WANG Feng~2(1.Power Engineering College,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China;2.China Ship Information Center,Beijing 100085,China);Analysis on the Ballistic Characteristics of Gliding Extended Range Projectile[J];Acta Armamentarii;2006-02
2 DING Song bin, WANG Zhong yuan, WANG Zheng lun (Power Eng. College, NUST, Nanjing, 210094 China);The Study on Horizon Gliding Range of Gliding Range-Assited Projectile With Fins[J];;2000-04
3 TU Sheng-yuan ZHANG Ben Ammunition Engineering department of Ordnance Engineering College,Shijiazhuang 050003,China WANG Jun-bo Equipment Technology Institute of Artillery and Aerial Defence,Beijing 100012,China FU Ting-wei 71521 Military Group,Xinxiang 45002,China;Simulation Research of Trajectory of Gliding Range-extended Projectile[J];Journal of Projectiles,Rockets,Missiles and Guidance;2005-SA
4 SHI Jin-guang WANG Zhong-yuan TU Si-hua ((Power Eng.College,NUST,Nanjing 210094,China);The Calculating Method on a Suitable Angle of Lift-Canards of Gliding Extended Range Projectile[J];Journal of Projectiles,Rockets,Missiles and Guidance;2005-SC
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 Ding Songbin Wang Zhongyuan (Power Engineering School, NUST, Nanjing, 210094);ENERGY ANALYSIS METHOD FOR THE GLIDING TRAJECTORY OF A PROJECTILE[J];Acta Armamentarii;2002-01
2 WANG Jun,LU Fu-gang(No.203 Research Institute of China Ordnance Industries,Xi'an 710065,Shaanxi, China);Study on Pointing Error of Seeker[J];Acta Armamentarii;2009-03
3 WANG Xiao-na1,SHANG An-li2,WANG Xiang-jun1(1.College of Electrical and Information Engineering,Naval University of Engineering,Wuhan 430033,Hubei,China;2.Research Institute of Power Electronic Technology,Naval University of Engineering,Wuhan 430033,Hubei,China);Study on Application of Second-order Sliding Mode Control Theory to Gliding Extended Range Projectiles[J];Acta Armamentarii;2010-01
4 XIU Guan1,2,WANG Liang-ming1,SUN Rui-sheng1,YANG Rong-jun1(1.School of Energy and Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China; 2.Aerospace System Engineering Shanghai,Shanghai 201108,China);Research on a Fast Nonlinear Model Predictive Control Law[J];Acta Armamentarii;2011-10
5 BU Kui-chen1,2,LIU Li1 (1.College of Mechatronics Engineering,BIT,Beijing 100081,China; 2.China Academy of Launch Vehicle Technology System Engineering Division,Beijing 100076,China);Trajectory Design of Scanning Search Phase for MMW Terminal Guided Munition[J];Journal of Ballistics;2007-03
6 ZHENG Yousheng1,2,YANG Jianying1,TANG Dilian3,ZHOU Haiying4 (1Peking University,Beijing 100871,China;2Hongdu Aviation Industry Group Ltd,Nanchang 330024,China; 3College of Civil and Environmental Engineering,East China Institute of Technology,Jiangxi Fuzhou 344000,China; 4Yangzi College,East China Institute of Technology,Nanchang 330013,China);Optimization Design of Control Phase Trajectory About Extended Range Guided Projectile[J];Journal of Projectiles,Rockets,Missiles and Guidance;2010-06
7 ZHENG You-sheng,WANG Liang-ming(School of Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,China);Modeling and Simulating of Rocket Projectile Dynamic Vertical Launch[J];Flight Dynamics;2008-02
8 ZHOU Hao,CHEN Wan-chun,YIN Xing-liang(School of Astronautics,BUAA,Beijing 100083,China);The Scheme Design of Extended-Range Trajectory for Air to Surface Missile[J];Flight Dynamics;2008-03
9 LI Yan1,WANG Zhong-yuan1,DING Chuan-bing2(1.School of Energy and Power Engineering,NUST,Nanjing 210094,China; 2.China Ship Development and Design Center,Shanghai 201108,China);Study on Error Correction Method for Navigation System of Gliding Extended-range Projectile[J];Journal of Ballistics;2012-04
10 LI Tiepeng;WANG Zhongyuan;CHEN Qi;QIAO Lei;QIAO Xiangxin;Navy Armament Division;School of Energy and Power Engineering,NUST;School of Equipment Engineering,Shenyang Ligong University;;Study of Gliding Trajectory Optimization Algorithm Based on Gauss Pseudospectral Method[J];Journal of Projectiles,Rockets,Missiles and Guidance;2014-02
【Co-references】
Chinese Journal Full-text Database 6 Hits
1 Tang Liang1,Yang Jianmin2,Chen Fengyu1(1.Beijing Institute of Astronautical Systems Engineering,Beijing,100076; 2.China Academy of Launch Vehicle Technology,Beijing,100076);Trajectory Optimization with Multi-constraints for a Lifting Reentry Vehicle[J];Missiles and Space Vehicles;2013-01
2 ZHANG Peng-cheng1,LI Xin-guo2(1.School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China 2.United Simulation Center of Aerospace Transportation System,Northwestern Polytechnical University,Xi’an 710072,China);Base on trajectory optimization of glide phase with GPM for hypersonic glide vehicle[J];Electronic Design Engineering;2013-15
3 YANG Xiu-xia,ZHANG Yi,SHI Jian-hong,GAI Jun-feng(Department of Control Engineering,NAAU,Yantai Shangdong 264001,China);A Survey of Boost-Glide Aircraft Trajectory Design[J];Journal of Naval Aeronautical and Astronautical University;2012-03
4 SUN Yong,DUAN Guang-ren,ZHANG Mao-rui,ZHANG Ze(Center for Control Theory and Guidance Technology,Harbin Institute of Technology,Harbin 150001,China);Modified aerodynamic coefficient models of hypersonic vehicle in reentry phase[J];Systems Engineering and Electronics;2011-01
5 YONG En-mi,TANG Guo-jin,CHEN Lei (College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073,China);Rapid Trajectory Optimization for Hypersonic Reentry Vehicle Via Gauss Pseudospectral Method[J];Journal of Astronautics;2008-06
6 Li Yu,Cui Naigang (Harbin Institute of Technology,Harbin 150001,China);Reachable Domain Optimization for Intercontinental Boost-Glide Missile[J];Tactical Missile Technology;2010-01
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