| [1] |
WANG Yun-Peng, JIE Yong-Chun.
[J]. , 2018, 44(5): 22-29.
|
| [2] |
ZHENG Hai-Chao, HE Jun, CHEN Long-Hai.
[J]. , 2018, 44(4): 8-15.
|
| [3] |
LI Rong, PANG Jie, CHAO Ning.
[J]. , 2018, 44(4): 66-71.
|
| [4] |
WANG Min, WANG Si-Ye.
Thruster Configuration Problem Based on Regional Average Fuel Consumption
[J]. , 2018, 44(1): 51-55.
|
| [5] |
LI Mao-Mao.
Mars Optimal Entry Guidance with Constrained Control and Uncertainty
[J]. , 2017, 43(5): 7-13.
|
| [6] |
HAO Yun-Cai.
Technical Progress and Application of Space Optical Sensor
[J]. , 2017, 43(4): 8-18.
|
| [7] |
WEI Yan-Ming, LIU Xu-Hui, FAN Zi-Chen.
The Low Frequency Vibration Suppression and Control of Satellite
Based on Disposable Micro Impulse Thruster Array
[J]. , 2017, 43(3): 1-6.
|
| [8] |
XUE Chao, TAN Shu-Ping, LIU He-Long.
Librational Controller Design for a Tethered Satellite
System during Orbital Maneuvering
[J]. , 2017, 43(2): 21-27.
|
| [9] |
WANG Xin-Min, CHU Yong-Hui, ZHANG Jun-Ling, YUAN Jun.
On the Influence of Rotatable Payload and control for Satellite Attitude
[J]. , 2016, 42(5): 14-.
|
| [10] |
WU Zhi-Gang, LIU Yu-Liang, ZHANG Kai-Ming, WU Shu-Nan.
The Influences of Higher Order Gravitational Force and
Torque to the Motion of Space Solar Power Station
[J]. , 2016, 42(4): 1-.
|
| [11] |
WANG You-Yi, TANG Liang, HE Ying-Zi.
Dynamic Modeling and Decoupled Control of Ultra Quiet Platform
[J]. , 2016, 42(4): 6-.
|
| [12] |
ZHANG Xiao-Wei, WANG Jing-2, YUAN Yan-Hong, DAI Wei-Zong, HUANG Jing-Mei, ZHANG Ze-Tao.
HardwareintheLoop Simulation System for Rapid Validation of High Accuracy Space Orbit Control Mission
[J]. , 2016, 42(4): 42-.
|
| [13] |
LU Rui, WU Yan-Peng.
An Approach of Star Image Simulation for Strapdown Star Sensor
[J]. , 2016, 42(4): 57-.
|
| [14] |
HU Hai-Xia, TANG Liang, SHI Heng, DONG Wen-Qiang.
Research and Development of Numerical Simulation Techniques for Spacecraft GNC System
[J]. , 2016, 42(3): 1-8.
|
| [15] |
ZHANG Yang, WANG Dian-Jun, ZHU Zhi-Bin, GAO En-Yu.
Relative Navigation Algorithm for GEO Noncooperative Satellites Based on LineofSight Measurement and Orbit Prediction
[J]. , 2016, 42(3): 21-26.
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