[1] |
XIE Yongchun, CHEN Changqing, LI Xiangyu, LI Zhenyu.
A guidance strategy for rendezvous and docking to the space station in the Earth-Moon NRHO orbit
[J]. Chinese Space Science and Technology, 2024, 44(4): 29-39.
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[2] |
ZHOU Siyu, GU Yingying, YANG Yuetang, SHI Liheng, MA Yuxuan, ZHU Feihu, ZHANG Yunfang, WU Guanhao.
Space application and test design of dual-comb ranging technique
[J]. Chinese Space Science and Technology, 2024, 44(3): 127-135.
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[3] |
WANG Xiaoxue, LIU Chuankai, WANG Baofeng, TANG Geshi, WANG Jia, GUO Xiangyan.
Fast and stable tracking method for space manipulator capturing dynamictarget#br#
[J]. Chinese Space Science and Technology, 2018, 38(1): 18-28.
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[4] |
CHEN Shao-Wu, DONG Guang-Liang, FAN Min, LI Hai-Tao, HAO Wan-Hong.
Relative Position and Velocity Error Covariance Analysis of Two Spacecraft in Lunar Orbit Rendezvous and Docking
[J]. Chinese Space Science and Technology, 2014, 34(5): 32-40.
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[5] |
LI Jing, WANG Hui-南, LIU Hai-Ying.
Plucker Linear Based Relative Position and Attitude Determination Algorithm for RVD
[J]. Chinese Space Science and Technology, 2013, 33(1): 69-74.
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[6] |
JI Qiang, LUO Yi-Jun, LI Jin, TIAN Mao.
Phase Interferometer Method for the Actual Angle measure
[J]. Chinese Space Science and Technology, 2012, 32(1): 72-76.
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[7] |
WEI Xi-Qing, SONG Shen-Min.
Vision-aided Attitude Determination for Air-bearing Simulator of Rendezvous and Docking
[J]. Chinese Space Science and Technology, 2011, 31(5): 41-47.
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[8] |
WANG Xiao-Liang, SHAO Xiao-Wei, GONG De-Ren, DUAN Deng-Ping.
An Adaptive Approach to Vision Measurement for Rendezvous and Docking with Non-cooperative Target in Space
[J]. Chinese Space Science and Technology, 2011, 31(3): 76-83.
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[9] |
JING Wu-Xing, CHEN Wei-Yue.
Fuel-optimal Precise Rendezvous Guidance Law in Elliptical Reference Orbit with J2 Perturbation
[J]. Chinese Space Science and Technology, 2011, 31(2): 16-24.
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[10] |
LU Wei, HUANG Jia-Rong, ZHONG Qi.
External Heat Flux on Manned Transport Spacecraft with Multiple Modes and Attitudes
[J]. Chinese Space Science and Technology, 2011, 31(1): 25-32.
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[11] |
WANG Da-Peng, LIU Yu-Qiang, CHEN Shao-Long, LIU Yong-Jian.
Error Analysis for Rendezvous and Docking with Linear Covariance Method
[J]. Chinese Space Science and Technology, 2011, 31(1): 48-55.
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[12] |
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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[13] |
SONG Shen-Min, ZHANG Da-Wei, PEI Run.
Guidance for Dynamic Obstacle Avoidance of Autonomous Rendezvous and Docking with Non-Cooperative Target
[J]. Chinese Space Science and Technology, 2010, 30(6): 39-48.
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[14] |
Zhong Rui Xu Shijie(School of Astronautics,Beihang University Beijing 100191).
Simple Tension Control Strategy for Variable Length Tethered Satellite System
[J]. Chinese Space Science and Technology, 2009, 29(06): 66-73.
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[15] |
Pan Hailin (Beijing Institute of Control Engineering,Beijing 100080) Hong Ruzhen (The University of Alabama in Huntsville USA).
Effect of Baffles on Sloshing Modulated Forces and Torques Responsed to Input Orbital Accelerations in Microgravity
[J]. Chinese Space Science and Technology, 2000, 20(01): -.
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