[1] |
MA Ming-Chao, GUO Liang, ZHANG Xu-Sheng, WU Qing-Wen.
CharacteristicsAnalysisofaOnewayMicroExpansionTypeHeatSwitchforSpaceApplication
[J]. Chinese Space Science and Technology, 2015, 35(6): 48-.
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[2] |
GUI Xiao-Hong, SONG Xiang-E.
TransientThermalAnalysisofHeatPipeReceiverunderMicrogravity
[J]. Chinese Space Science and Technology, 2015, 35(4): 46-52.
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[3] |
XU Xiao-Hui, HU Shao-Lin, GUO Xiao-Hong, ZHAO Zong-Yu.
SpacecraftTT&CSchedulingModelsandAlgorithms
[J]. Chinese Space Science and Technology, 2014, 34(3): 32-37.
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[4] |
XIAO Xin-Xin, LI Wen-Hao, ZHANG Heng, LIU Kai-Lei.
LEOSpacecraftMagnetismPropulsionandItsCapabilityEstimation
[J]. Chinese Space Science and Technology, 2013, 33(6): 67-73.
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[5] |
FU Jun, CAI Hong, ZHANG Shi-Feng.
Research on Aeroassisted Orbital Transfer between Elliptical Orbits
[J]. Chinese Space Science and Technology, 2012, 32(3): 64-71.
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[6] |
LUO Nan, XU Lu-Ping, ZHANG Hua.
Method of Autonomous Celestial Navigation Based on UKF and Information Fusion
[J]. Chinese Space Science and Technology, 2012, 32(2): 1-9.
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[7] |
WEI Peng-Xin, JING Wu-Xing, GAO Chang-Sheng.
Quaternion Method with Modified Constraint Equation for Nonsingular Orbital Elements
[J]. Chinese Space Science and Technology, 2012, 32(1): 66-71.
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[8] |
LIU Yong-Jian, LIU Yu-Qiang, SHI Jun, TAN Chun-Lin.
Numerical Optimization for Spacecraft Module Identification
[J]. Chinese Space Science and Technology, 2012, 32(1): 77-83.
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[9] |
ZHU Zhi-Bin, LI Guo, HE Ying-Zi, WEI Chun-Ling.
Relative Cooperative Attitude and Position Control of Fractioned Spacecraft Based on Iterative Optimization
[J]. Chinese Space Science and Technology, 2011, 31(2): 1-8.
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[10] |
NING Xian-Wen, ZHANG Jia-Xun.
Spacecraft Thermal Control Technology Based onVariable Frequency Pump
[J]. Chinese Space Science and Technology, 2011, 31(2): 47-52.
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[11] |
YUE Xiao-Kui, YUAN Yun-Xia.
Transfer Matrix for Relative Dynamics in Elliptic Orbit
[J]. Chinese Space Science and Technology, 2011, 31(1): 42-47.
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[12] |
JIN Lei, XU Shi-Jie.
Dynamics Modeling and Low Rate Control ofGimbal Servo System for Single Gimbal Control Moment Gyro
[J]. Chinese Space Science and Technology, 2010, 30(6): 1-10.
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[13] |
LI Xiao-Jie, DU Lan, HUANG Jin, PAN Ling.
CEI based Real time Orbit Determination of Spacecraft Rendezvous and Docking in the Course of Long Distance Navigation
[J]. Chinese Space Science and Technology, 2010, 30(6): 24-30.
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[14] |
Han Zengyao Qu Guangji (Beijing Institute of Spacecraft System Engineering,Beijing 100086).
Application of Noise Analysis on Solar Array by Statistical Energy Analysis
[J]. Chinese Space Science and Technology, 2001, 21(01): -.
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