2016 Issue 4
..............page:1-4
Attitude Maneuver Compensation Method on Lunar Imaging for Optical Remote Sensing Satellite
GAO Han;,BAI Zhaoguang;,LU Chunling;,DI Guodong;
GAO Han;,BAI Zhaoguang;,LU Chunling;,DI Guodong;
..............page:5-12
Study on Attitude Maneuver Strategy of Spotlight Mode of Agile SAR Satellite
HAN Xiaolei;,ZHANG Qingjun;,LIU Jie;,ZHANG Running;,YUAN Zhi;
HAN Xiaolei;,ZHANG Qingjun;,LIU Jie;,ZHANG Running;,YUAN Zhi;
..............page:13-19
Strategy of GEO Electric Propulsion Satellite Orbit Drift
ZHAO Yiping;,LI Feng;,JING Yaoxiang;,LI Dawei;
ZHAO Yiping;,LI Feng;,JING Yaoxiang;,LI Dawei;
..............page:20-26
Attitude Maneuver Control Method for Agile Satellite Based on Input Shaping
ZHOU Weimin;,LIAO Ying;,YANG Yajun;,ZHU Qinghua;
ZHOU Weimin;,LIAO Ying;,YANG Yajun;,ZHU Qinghua;
..............page:27-32
Optimization Analysis of Electric Thrusters Installation Location on GEO Satellite
LI Qiang;,ZHOU Zhicheng;,YUAN Jungang;,WANG Min;
LI Qiang;,ZHOU Zhicheng;,YUAN Jungang;,WANG Min;
..............page:33-39
Decoupled Loading Method of Disturbance Sources for Spacecraft Micro-vibration Analysis
ZOU Yuanjie;,WANG Zeyu;,GE Dongming;
ZOU Yuanjie;,WANG Zeyu;,GE Dongming;
..............page:40-47
An Intelligent Control Strategy of Spacecraft Electric Heating
ZHANG Hongbo;,PAN Yuqian;,FENG Wenjing;,WANG Haitao;
ZHANG Hongbo;,PAN Yuqian;,FENG Wenjing;,WANG Haitao;
..............page:48-53
Analysis on Key Techniques of Onboard Autonomous Mission Management System of Optical Agile Satellite
ZHU Jianbing;,WANG Luyuan;,ZHAO Wei;,TIAN Hexiang;
ZHU Jianbing;,WANG Luyuan;,ZHAO Wei;,TIAN Hexiang;
..............page:54-59
Design of Real-time Processing System for Transmission Data of Multi-satellite and Multi-mission
YANG Jiasen;,MENG Xin;,WANG Chunmei;
YANG Jiasen;,MENG Xin;,WANG Chunmei;
..............page:60-66
Research on Application of ARINC659 Bus in Spacecraft Avionics System
LIU Weiwei;,CHENG Bowen;,WANG Luyuan;,YU Minfang;
LIU Weiwei;,CHENG Bowen;,WANG Luyuan;,YU Minfang;
..............page:67-73
A Design Method for Radiation Hardened Space-borne AISC Based on FPGA
CHANG Kewu;,WANG Haitao;,ZHANG Gong;,WANG Luyuan;
CHANG Kewu;,WANG Haitao;,ZHANG Gong;,WANG Luyuan;
..............page:74-80
A Radiation Hardened Method Based on COTS Components
LIANG Jian;,ZHANG Running;,ZHAO Shuai;
LIANG Jian;,ZHANG Running;,ZHAO Shuai;
..............page:81-86
..............page:87-94
Reusable Thermal Protection System for Orbital Test Vehicle X-37B
ZHOU Zhiyong;,MA Bin;,ZHANG Cui;,HAN Xiuzhu;,LIU Feng;,DONG Yanzhi;
ZHOU Zhiyong;,MA Bin;,ZHANG Cui;,HAN Xiuzhu;,LIU Feng;,DONG Yanzhi;
..............page:95-101
Research on Orion Electronic System
CHENG Bowen;,LIU Weiwei;,HE Xiongwen;,YAN Dong;
CHENG Bowen;,LIU Weiwei;,HE Xiongwen;,YAN Dong;
..............page:102-107
Practice and Inspiration in Development of Integrated Electronic Subsystem Software for Test Satellite of Beidou Navigation Satellite System
CHANG Kewu;,JIA Weisong;
CHANG Kewu;,JIA Weisong;
..............page:108-112
Methods of Damage Location and Evaluation for Satellite Structure Based on Frequency Response Principle Component
FENG Yanjun;,SHI Chuanqian;,ZHOU Yu;,ZHAO Fagang;,ZHOU Xubin;
FENG Yanjun;,SHI Chuanqian;,ZHOU Yu;,ZHAO Fagang;,ZHOU Xubin;
..............page:113-120
Research on Strength Testing of Solar Wing Substrate for Lunar Lander
LIU Shaofeng;,SHANG Hongjun;,YANG Qiaolong;,REN Shouzhi;,LIANG Dongping;
LIU Shaofeng;,SHANG Hongjun;,YANG Qiaolong;,REN Shouzhi;,LIANG Dongping;
..............page:121-126
Simulation Analysis and Test Verification of Impact Load for Solar Wing Pyrotechnic Release
YAN Qingqing;,YAN Zehong;,TAN Limeng;,PU Hailing;,LI Xuan;
YAN Qingqing;,YAN Zehong;,TAN Limeng;,PU Hailing;,LI Xuan;
..............page:127-132
..............page:133-140,封2