1000-1328
2016 Issue 8
A Method of Pulsar-Based Dynamic Orbit Determination in the Earth-Fixed Reference Frame for Near-Earth Spacecraft
HUANG Liang-wei;,SHUAI Ping;,ZHANG Xin-yuan;,LIN Qing-qing;
HUANG Liang-wei;,SHUAI Ping;,ZHANG Xin-yuan;,LIN Qing-qing;
..............page:895-900
Characteristics of Bow Shock for a Forward-Facing Cavity
WANG Gang;,MA Xiao-wei;,JIANG Tao;,GONG Hong-ming;,KONG Rong-zong;,YANG Yan-guang;
WANG Gang;,MA Xiao-wei;,JIANG Tao;,GONG Hong-ming;,KONG Rong-zong;,YANG Yan-guang;
..............page:901-907
Analytical Method for Ground Track Manipulation Using Impulse Thrust Based on J2 Perturbation
SHENG Jing;,ZHANG Gang;,GENG Yun-hai;
SHENG Jing;,ZHANG Gang;,GENG Yun-hai;
..............page:908-916
Disturbance Characteristics Analysis of Magnetically Suspended and Mechanical Flywheels
DENG Rui-qing;,ZHAO Yan;,FANG Jian-cheng;,ZHANG Da-chuan;
DENG Rui-qing;,ZHAO Yan;,FANG Jian-cheng;,ZHANG Da-chuan;
..............page:917-923
Takeover Control of Attitude Maneuver for Failed Spacecraft
HUANG Pan-feng;,WANG Ming;,CHANG Hai-tao;,MENG Zhong-jie;
HUANG Pan-feng;,WANG Ming;,CHANG Hai-tao;,MENG Zhong-jie;
..............page:924-935
Integrated Guidance and Control Design Method Considering Channel Coupling
SUN Xiang-yu;,CHAO Tao;,WANG Song-yan;,MA Ping;
SUN Xiang-yu;,CHAO Tao;,WANG Song-yan;,MA Ping;
..............page:936-945
A New Method for Orbit and Attitude Coupling Control Problem of Flexible Spacecraft Based on Dual Quaternions
YANG Yi-dai;,JING Wu-xing;,ZHANG Zhao;
YANG Yi-dai;,JING Wu-xing;,ZHANG Zhao;
..............page:946-956
Command Filtered Backstepping Control for Hypersonic Vehicle
DONG Chao-yang;,LU Yao;,WANG Qing;
DONG Chao-yang;,LU Yao;,WANG Qing;
..............page:957-963
Guidance and Attitude Control System Design for Hypersonic Vehicle in Dive Phase
WANG Jian-hua;,LIU Lu-hua;,TANG Guo-jian;
WANG Jian-hua;,LIU Lu-hua;,TANG Guo-jian;
..............page:964-973
PN Guidance Law Identification Using Multi-Model Adaptive Estimation
ZOU Xin-guang;,ZHOU Di;,DU Run-le;,LIU Jia-qi;
ZOU Xin-guang;,ZHOU Di;,DU Run-le;,LIU Jia-qi;
..............page:974-983
Glide Guidance Method for Maneuverable Reentry Vehicle Against Time-Sensitive Target
CHEN Si-yuan;,XIA Qun-li;,LI Qiang;
CHEN Si-yuan;,XIA Qun-li;,LI Qiang;
..............page:984-991
A Mixed Integer Predictive Controller with Multi-Constraint for Free-Floating Space Robots
ZONG Li-jun;,LUO Jian-jun;,WANG Ming-ming;,YUAN Jian-ping;
ZONG Li-jun;,LUO Jian-jun;,WANG Ming-ming;,YUAN Jian-ping;
..............page:992-1000
A Singularity Escape Method for SGCMG System
LIU De-qing;,WU Jing-yu;,CAO Hong-lei;
LIU De-qing;,WU Jing-yu;,CAO Hong-lei;
..............page:1001-1005
Performance Optimization and Control for Mission-Oriented Electric Propulsion Spacecraft
ZHANG Zhong-lei;,DING Yong-jie;,YU Da-ren;
ZHANG Zhong-lei;,DING Yong-jie;,YU Da-ren;
..............page:1006-1014
Mechanical Design and Analysis of Joint Quick Exchange Interface for Space Manipulator
SHI Shi-cai;,HE Yang;,LI Rong;,LIU Hong;
SHI Shi-cai;,HE Yang;,LI Rong;,LIU Hong;
..............page:1015-1022
The Effect of Orbital Parameters on the Solar Flux Density of the Alpha Magnetic Spectrometer
XIE Min;,GAO Jian-min;,DU Qian;,WU Shao-hua;,QIN Yu-kun;
XIE Min;,GAO Jian-min;,DU Qian;,WU Shao-hua;,QIN Yu-kun;
..............page:1023-1030