| [1] |
XING Linfeng，SUN Chengqi，TANG Liang. VSCMGS-Based Steering Law Design for a High Attitude Stability Agile Satellite[J]. , 2008, 34(6): 24
-28
. |
| [2] |
ZHAO Jiang-Tao-； Li-Guo. Torque Compensation for Payload Disturbance of a Flexible Satellite with High Stability[J]. , 2011, 37(4): 7
-12
. |
| [3] |
Wang-Yong-； Gong-Yu-Lian-； Wang-Li-Jiao. MIMO Characteristic Model Based Adaptive Attitude Control for Hypersonic Vehicle[J]. , 2011, 37(4): 13
-18
. |
| [4] |
GONG Jian-； Yang-Hua-； Zhao-Wei-； Qiao-Lei-； . Knowledge Inference Based Self Fault Diagnosis Method for Spacecraft[J]. , 2011, 37(4): 19
-23
. |
| [5] |
LIU Cheng-Rui, XU Chun, WANG Zhi-Hua. Analysis Method of Gyro Random Drift Based on Correlation Coefficient AR model[J]. , 2011, 37(4): 31
-35
. |
| [6] |
WANG Shu-Yi, WEI Chun-Ling, LIU Qi-Rui- . A Quick Attitude Maneuver Algorithm for Agile Satellites[J]. , 2011, 37(4): 36
-40
. |
| [7] |
Ke-Qi-； Wang-Yong-； Wei-Chun-Ling-； . A Way to Improve Attitude Control Accuracy for Momentum Biased Satellite[J]. , 2011, 37(4): 41
-44
. |
| [8] |
Qiao-Guo-Dong-； Li-Kang-； Zeng-Hai-Bo. Robust H∞ Filter Algorithm for Nonlinear Uncertain System[J]. , 2011, 37(4): 45
-48
. |
| [9] |
Wu-Hao-； Yang-Ye. Dynamic Inversion Reentry Guidance Based on RCMAC Network[J]. , 2011, 37(4): 49
-53
. |
| [10] |
Li-Yong-； Hu-Qi-； Pan-Hai-Lin-； Geng-Yong-Bing-； Ding-Feng-Lin. Numerical Simulation and Ground Test Research on Orbital Refueling Process[J]. , 2011, 37(4): 54
-57
. |
|
