[1] |
LIU Qi-Hai, GONG De-Zhu, HUA Bao-Cheng, ZHONG Jun, ZHENG Yan, ZHAO Chun-Hui- .
New Generation CameraType Rendezvous and Docking Sensor
[J]. , 2018, 44(2): 56-61.
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[2] |
CHEN Zhi-Hua, XIE Yong-Chun.
Stability Analysis of the ClosedLoop System of a PhasePlane Controlled Rigid Satellite
[J]. , 2018, 44(1): 1-14.
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[3] |
YAN Han, HE Ying-Zi.
DragTracking Guidance for Entry Vehicles with Finite Time
[J]. , 2018, 44(1): 38-44.
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[4] |
LIU Ji-Li, LI Jian-Peng, WU Zhi-Zhong, LI Kai- .
SelfCompensation of Bias Temperature Drift in Hemispherical Resonator Gyro
[J]. , 2018, 44(1): 69-73.
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[5] |
LIANG Jing-Jing, XIE Yong-Chun .
Design Method of Safe FlyAround Trajectory Based on Rectangular KeepOutZone
[J]. , 2018, 44(1): 45-50.
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[6] |
LU Xin, LI Chun-Yan, LI Xiao, SUN Da-Kai, XIA Meng-Qi.
Current Situation and Development Trends of Starlight Navigation Technology
[J]. , 2017, 43(4): 1-8.
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[7] |
ZHENG Xun-Jiang, YE Zhi-Long, YANG Qin-Li, SUN Shuo-Dong.
A Correction Method of NonUniformity Pixel Error Applied to
Star Sensor Based on MultiFrame Correlation Filtering
[J]. , 2017, 43(4): 31-36.
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[8] |
GENG Jie, 吕Nan , WANG Tao, GONG Jing-Gang.
A Novel FiniteTime Sliding Mode Attitude Controller for Spacecraft
[J]. , 2016, 42(4): 30-.
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[9] |
CHEN Yang.
A Nominal Trajectory Method Combined with PD Control in TAEM Phase
[J]. , 2016, 42(3): 58-62.
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[10] |
ZHAO Yuan, MO Ya-Nan, LV Zheng-Xin .
Error Analysis and Modify Method of the New Coded Sun Sensor
[J]. , 2016, 42(2): 38-42.
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[11] |
LONG Ye, LIU Yi-Wu.
An Online Desensitized Trajectory Design Method for Mars Entry Guidance
[J]. , 2016, 42(2): 20-25.
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[12] |
ZHANG Xiao-Lei, ZHENG Jian-Hua, GAO Dong, QIAN Hang.
Correction of the Relative Orbit States Based on InterSatellite
Ranging for MicroSatellites Formation
[J]. , 2015, 41(3): 42-47.
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[13] |
GUAN Xin, CHEN Shou-Lei, CUI Ying-Hui, TANG Liang, ZHENG Gang-Tie.
Dynamics Coupling and Integrated Design in Vibration Isolation and Attitude Control Design of UltraQuiet Agile Satellites
[J]. , 2015, 41(1): 21-25.
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[14] |
WANG Zhi-Wen, ZHANG Hong-Hua.
Error Analysis Based on Linear Covariance for Lunar Powered Ascent Phase
[J]. , 2014, 40(3): 25-31.
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[15] |
LIU Zhi-Yong, HE Ying-Zi, CAI Biao, CHENG Ying-Kun.
Attitude Control for NonCooperative Target Tracking Based on Nonlinear Observer
[J]. , 2013, 39(5): 19-23.
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