1006-3242
2014 Issue 2
Design and Realization of MEMS Integrated Navigator Based on SOPC
LIANG Haibo;,LIU Zhihua;,SI Wenjie;,XIAO Changyi;
LIANG Haibo;,LIU Zhihua;,SI Wenjie;,XIAO Changyi;
..............page:3-8
Inertial Platform Modeling and Simulation Based on Centrifuge Test with a Rotating Table
GUO Tao;,LIANG Luyang;,WU Hao;,YANG Ye;
GUO Tao;,LIANG Luyang;,WU Hao;,YANG Ye;
..............page:9-12,17
An Automated Way of Testing for Flying Attitude Control Functions
XU Chunlai;,ZHANG Shu;
XU Chunlai;,ZHANG Shu;
..............page:13-17
Data Collection of Accelerometer in Strapdown Inertial Navigation System
LIU Qingqing;,TAN Xinhong;,ZHOU Lu;
LIU Qingqing;,TAN Xinhong;,ZHOU Lu;
..............page:18-22
Influence Analysis of Harmonic Gear to SGCMG Gimbal Rate Control
JIA Yinghong;,JIN Lei;,LIU Baoyu;
JIA Yinghong;,JIN Lei;,LIU Baoyu;
..............page:23-28,34
Estimation of Ballistic Wind Speed Base on Aerodynamic Parameter Identification
CHEN Chang;,TIAN Feng;,XIAO Liangang;,ZHANG Jisheng;,ZHANG Yanru;
CHEN Chang;,TIAN Feng;,XIAO Liangang;,ZHANG Jisheng;,ZHANG Yanru;
..............page:29-34
..............page:35-40,96
Covering Capability Analysis of Terminal High Altitude ATBM System
LU Yingqi;,ZHANG Xiaokuan;
LU Yingqi;,ZHANG Xiaokuan;
..............page:41-45,96
Reconfigurable Allocation of Satellite Attitude Control System
CHEN Yuehua;,JIANG Bin;,LIU Chengrui;,XIANG Changyi;,YANG Hao;
CHEN Yuehua;,JIANG Bin;,LIU Chengrui;,XIANG Changyi;,YANG Hao;
..............page:46-52,59
The Relative Coupling Attitude and Orbit Control of Fast Fly-around with Monitoring Spacecraft
JIN Yongqiang;,KANG Zhiyu;,XIAO Yuzhi;,ZHANG Qingzhan;
JIN Yongqiang;,KANG Zhiyu;,XIAO Yuzhi;,ZHANG Qingzhan;
..............page:53-59
Relative Attitude Estimation for Space Non-cooperative Targets Based on Sequence of Monocular Images
DU Xiaoping;,HAO Gangtao;
DU Xiaoping;,HAO Gangtao;
..............page:60-67
Depleted Shutdown Closed Loop Guidance with Maximum Height and Reentry Angle Constraint
WANG Xiaohu;,ZHANG Zhijian;
WANG Xiaohu;,ZHANG Zhijian;
..............page:68-72
Stability Control for Station-Keeping Phase of Space Tether System Based on Standard Coefficient Method
LI Aijun;,LI Chao;,WANG Changqing;,ZABOLOTNOV Yuriy;
LI Aijun;,LI Chao;,WANG Changqing;,ZABOLOTNOV Yuriy;
..............page:73-77
Research on Electromechanical Driving Technology and Development of Novel Rudder Servo Load Simulator
CHEN Junjie;,HUANG Yuping;,WANG Yuexuan;,ZHANG Zhongzhe;,ZHAO Guoping;,ZHONG Yue;
CHEN Junjie;,HUANG Yuping;,WANG Yuexuan;,ZHANG Zhongzhe;,ZHAO Guoping;,ZHONG Yue;
..............page:78-86
Queuing Theory Based Complex Spectrum Environment Models in the Battlefield
LIN Jinyong;,MA Jifeng;,ZHANG Shuo;
LIN Jinyong;,MA Jifeng;,ZHANG Shuo;
..............page:87-90
Design Pattern Used in Software Reuse of Test Launch and Control System
MA Weihua;,MA Yingjin;,XIE Yuejiang;,YANG Zhe;
MA Weihua;,MA Yingjin;,XIE Yuejiang;,YANG Zhe;
..............page:91-96