[1] |
XU Jin, WANG Qiuping, LI Yao, SUN Ji, CHEN Lan, YU Xiaochuan, WANG Hai, TIAN Sen, DANG Xiaokang, WANG Yongta.
Mission analysis and design of Queqiao-2 communication relay payload
[J]. Chinese Space Science and Technology, 2025, 45(3): 41-55.
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[2] |
FENG Tao, ZAHNG Qingjun, LIN Kunyang, WANG Lipeng, ZHANG Qiao, YANG Jungang, XIAO Yong.
System design of spaceborne large aperture perimeter truss antenna
[J]. Chinese Space Science and Technology, 2025, 45(1): 24-33.
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[3] |
ZHANG Lihua, XIONG Liang, SUN Ji, CHEN Luojing, XIAO Chuan, ZHOU Wenyan, WANG Yong, LIU Wangwang, GUAN Yifeng, CHEN Tao, YU Xiaochuan, XU Jin, CHEN Guohui, CAO Xiaoping.
System design and validation of Queqiao-2 lunar relay communication satellite
[J]. Chinese Space Science and Technology, 2024, 44(5): 23-39.
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[4] |
BAI Zhaoguang, WANG Chongyu, FAN Dongdong, SUN Jiwen.
BF-1 satellite system design and technology characteristics
[J]. Chinese Space Science and Technology, 2022, 42(2): 108-116.
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[5] |
PAN Xiao, XU Ming.
Overview of non-Keplerian displaced orbits by low-thrust propulsion
[J]. Chinese Space Science and Technology, 2021, 41(4): 1-15.
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[6] |
CAO Haiyi, ZHANG Xinwei, ZHAO Chenguang, XU Chi, MO Fan, DAI Jun.
System design and key technolongies of the GF-7 satellite
[J]. Chinese Space Science and Technology, 2020, 40(5): 1-9.
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[7] |
ZHAN Panpan, CAO Yating, ZHANG Cuitao, LIN Xiangyu, GU Ming.
High functional density avionics system for satellites#br#
[J]. Chinese Space Science and Technology, 2020, 40(1): 87-.
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[8] |
YANG Chi-Hang, LIU Jiang-Kai, LONG Long- , SONG Huan, LI Long, ZHU Ling-Chao, YE Bing-Xu, CHEN Hong-Ru, ZHANG Hao.
Preliminary design and test of attitude control system for lunar CubeSats
[J]. Chinese Space Science and Technology, 2019, 39(4): 28-.
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[9] |
GU Zhen-Feng, WANG Zhao-Kui, ZHANG Yu-Lin.
Reduction of Gravitational Attraction Disturbance to Purely Gravitational Orbit Based on Satellite Spinning
[J]. Chinese Space Science and Technology, 2013, 33(4): 40-46.
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[10] |
JIANG Feng, WANG Hui-nan, HUANG Chao-Song.
Algorithm for Relative Position and Attitude of Formation Flying Satellites Based on Dual Quaternion
[J]. Chinese Space Science and Technology, 2012, 32(3): 20-26.
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[11] |
DUAN Chuan-Hui, DONG Yun-Feng.
Optimal Control of Spacecraft Fly-around Releasing Using Continuous Thrust Based on Gauss Pseudospectral Method
[J]. Chinese Space Science and Technology, 2011, 31(5): 18-24.
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[12] |
CHEN Zhi-Ming, LIU Hai-Ying, WANG Hui-Nan, FENG Cheng-Tao.
Rotating Formation Flying for Tethered Micro-satellites
[J]. Chinese Space Science and Technology, 2011, 31(1): 76-83.
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[13] |
WANG Da-Peng, TAN Chun-Lin, ZHANG Bai-Nan.
On-orbit Maintainability System Design forManned Spacecraft
[J]. Chinese Space Science and Technology, 2010, 30(5): 16-22.
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[14] |
Zhang Hao1,2 Li Mingtao1,2 Zhang Xiucheng1,2(1 Center for Space Science and Applied Research,Beijing 100190) (2 Graduate School of Chinese Academy of Science,Beijing 100190).
Error Analysis of the Relative Motion in Formation Flying Satellites Based on Two J_2 Perturbation Models
[J]. Chinese Space Science and Technology, 2010, 30(03): 25-30.
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[15] |
Bi Peng Luo Jianjun Zhang Bo(Northwestern Polytechnical University,Xi′an 710072).
Attitude Control Algorithm for Spacecraft Formation Flying Based on Network Synchronization
[J]. Chinese Space Science and Technology, 2010, 30(01): 46-51.
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