[1] |
PENG Yaqi, LI Chonghui, WANG Yiwen, WEI Wulei, DING Baichao, LIU Yangqian.
Error analysis and prediction of Klobuchar ionospheric model
[J]. Chinese Space Science and Technology, 2021, 41(1): 48-54.
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[2] |
ZHANG Tiangang,REN Tianpeng,XIE Jianfeng,LU Weitao,YIN Feifei.
Spacecraft attitude measurement based on samebeam interferometry
[J]. Chinese Space Science and Technology, 2019, 39(2): 19-26.
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[3] |
WANG Dapeng, ZHOU Weijing, CAO Jihong, ZHANG Shan, SHI Xiaoyun, HE Long.
A measurement method of dynamic thrust based on cantilever beam
[J]. Chinese Space Science and Technology, 2018, 38(5): 63-71.
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[4] |
XIA Zhong-Qiu, HUANG Qiao-Lin, HE Hong-Yan, YANG Yuan-Li, SUN Shi-Jun, YUE Chun-Yu.
Simulationandanalysisofstereogeolocationaccuracyofspacecamerabywhiskbroomimaging
[J]. Chinese Space Science and Technology, 2017, 37(2): 117-125.
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[5] |
XIA Meng, YANG Xiao-Niu.
Error Analysis and Moving Target Position for Spaceborne SAR-DPCA with Three-channel
[J]. Chinese Space Science and Technology, 2011, 31(2): 58-63.
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[6] |
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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[7] |
YU Hui, HU Shao-Lin, LI Ping.
Radar Data Error-correction Technique Based on Hilbert-Huang Transform
[J]. Chinese Space Science and Technology, 2010, 30(6): 57-63.
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[8] |
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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[9] |
Hu Di Dong Yunfeng(Beihang University,Beijing 100191).
Design of General-purpose Electric Simulator for Satellite Attitude and Orbit Control System Based on SOC
[J]. Chinese Space Science and Technology, 2010, 30(02): 24-30.
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[10] |
Yao Jing1 Gu Defeng2 Yi Dongyun2 Zhu Jubo2(1 College of Computer,National University of Defense Technology,Changsha 410073)(2 College of Science,National University of Defense Technology,Changsha 410073).
Modeling and Analysis of Spatial States and Inter-Satellite Baseline in Formation Flying Missions
[J]. Chinese Space Science and Technology, 2008, 28(06): 21-28.
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[11] |
Zhong Xingwang Chen Hao (Xi'an Institute of Space Radio Technology,Xi'an 710000).
Analysis and Correction Techniques of Movement Influence on Inter-Satellite Two-way Time Transfer
[J]. Chinese Space Science and Technology, 2007, 27(06): 54-58.
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[12] |
Liu Tao Xie Yongchun(Beijing Institute of Control Engineering,Beijing 100080).
Study of Relative Navigation Based on Relative Differential Pseudo Range of GPS
[J]. Chinese Space Science and Technology, 2007, 27(01): 1-8.
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[13] |
Wang Jiongqi Zhou Haiyin Zhao Deyong Wu Yi(National University of Defense Technology,Changsha 410073).
Mathematical Method for Orbit Determination Based on GEOSTAR System
[J]. Chinese Space Science and Technology, 2006, 26(05): 1-5+56.
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[14] |
Yan Rongxin Liu Ping Feng Qi Hong Xiaopeng Shi Lixia(China Academy of Space Technology,Beijing 100094).
Factor of Leak Detection for Pressure Decay
[J]. Chinese Space Science and Technology, 2006, 26(04): 37-41.
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[15] |
Zhu Zhuanmin~* Qiu Hongxing~(**) Xu Zongben~*(*Mathematical College of Xi′an Jiaotong University,Xi′an 710049)(**Nanjing Zijinshan Astronomical Observatory of China Academy of Sciences,Nanjing 210008).
The Error Estimate to the Single Circle Observation Data of Satellite
[J]. Chinese Space Science and Technology, 2005, 25(05): 29-33.
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