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Aerospace Contrd and Application
1674-1579
2016 Issue 2
New Generation of Star Tracker Baffle—CNT Baffle
HAO Yuncai;,YU Chengwu;,LIANG Shitong;,MEI Zhiwu;,QIAN Weizhong;
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page:1-7,31
Method of Mission Analysis for Solar Sail Exploration Based on STK
QIAN Hang;,ZHENG Jianhua;,WU Xia;,GAO Dong;,LIU Yufei;
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page:8-13,19
Friction Parameter Identification for High Stability SADA
CHENG Junbo;,ZHANG Qiang;,HU Gang;,YU Guoqing;,LU Dongning;
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page:14-19
An Online Desensitized Trajectory Design Method for Mars Entry Guidance
LONG Ye;,LIU Yiwu;
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page:20-25
Dynamic Modeling and Simulation of Flexible Space Manipulator Based on Vector Pairs Method
LIN Qian;,YUAN Jun;
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page:26-31
Effects of the Flexible Brackets on Flywheel Isolation System
CHEN Chen;,WANG Hong;,WU Dengyun;,FAN Yahong;,GUAN Xin;
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page:32-37
Error Analysis and Modify Method of the New Coded Sun Sensor
ZHAO Yuan;,MO Yanan;,LV Zhengxin;
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page:38-42
Robustness of an CP-FODT-Based Algorithm for Real-Time Data Processing
LIANG Hong;
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page:43-48
Design of Laser Diode Driving Circuit Used in Space Vision Measurement Subsystem
WANG Dongning;,ZHANG Lin;,HUA Baocheng;,ZHENG Yan;,GONG Dezhu;,ZHAO Chunhui;
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page:49-52,62
Improved Baffle Used for Star Sensor
LIANG Shitong;,ZHONG Hongjun;,LIU Jing;
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page:53-56
A Non-Affine Extension Method of Polyhedral Model Based on Dynamic Analysis
WANG Jianhua;,CHEN Zhaohui;
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page:57-62