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《Tactical Missile Technology》 2014-01
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Aerodynamic Modeling and Pneumatic Force /Reaction Combination Control System for Near Space Vehicle

Xu Xingguang;Li Shusheng;Wei Qingxin;Yang Guang;Huang Daoqing;Beijing Electro-mechanical Engineeing Institute;  
Aimed at variations of circumstances and aerodynamic characteristics for near space vehicle,a modeling idea of near space vehicle is discussed and control method is designed. Near space vehicle is simplified by the small perturbation linear model and the aerodynamic characteristics of the missile are analyzed. Two sets of control systems are designed. The ignition time and the jet flow are determined, and the aircraft are simulated by Matlab / Simulink. The results show that the controlled object has good dynamic and static characteristics.
【CateGory Index】: V249.1
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【Citations】
Chinese Journal Full-text Database 1 Hits
1 HU Wei-jun,ZHOU Jun(Institute of precise guidance and control,Northwestern Polytechnical University,Xi'an Shanxi 710072,China);A Design Method of Controller for Reaction Control System in High Atmosphere[J];计算机仿真;2010-03
【Co-citations】
Chinese Journal Full-text Database 2 Hits
1 Xu Xingguang;Li Shusheng;Wei Qingxin;Yang Guang;Huang Daoqing;Beijing Electro-mechanical Engineeing Institute;;Aerodynamic Modeling and Pneumatic Force /Reaction Combination Control System for Near Space Vehicle[J];战术导弹技术;2014-01
2 @XU Xing-guang$Beijing Institute of Mechanical and Electronic Engineeing!Beijing 100074 @LI Shu-sheng$Beijing Institute of Mechanical and Electronic Engineeing!Beijing 100074 @YANG Guang$Beijing Institute of Mechanical and Electronic Engineeing!Beijing 100074;A combination of pneumatic force and reaction control system for near space vehicle using MATLAB/SIMULNK[J];战术导弹控制技术;2013-02
【Secondary Citations】
Chinese Journal Full-text Database 5 Hits
1 QIAN Cheng-shan1,2,WU Qing-xian1,JIANG Chang-sheng1,ZHOU Li1(1.College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;2.College of Information and Control, Nanjing University of Information Science and Technology,Nanjing 210044,China);Flight control for an aerospace vehicle's reentry attitude based on thrust of reaction jets[J];航空动力学报;2008-08
2 Zhang Yang Li Kefeng Zhang Qingzhen Ren ZhangBeijing University of Aeronautics and Astronautics,Beijing 100083,China;Reaction Control System of RLV Blended Control in Re-entry Mode[J];航天控制;2008-03
3 Fang Yuanpeng(31st Research Lab,Chengdu Aircraft Design and Research Institute,Chengdu 610041,China);Reaction Control System Control Method for Reusable Launch Vehicle[J];航空学报;2008-S1
4 Ji Pengfei,Zhou Jun,Hu Weijun (Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi′an 710072,China);Two Different Methods of JSL Reconfiguration for Reusable Launch Vehicle′s Reentry Phase[J];西北工业大学学报;2007-06
5 HU Wei-jun,ZHOU Jun(Astronautics College,Northwestern Polytechnical University,Xi'an 710072,China);Research on Revised Pulse Wide Modulation of Reaction Control System for Reusable Launch Vehicle[J];弹箭与制导学报;2006-04
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