[1] |
ZHANG Junhua, CHEN Jianlin, SUN Chong, YUAN Jianping.
Onboard orbit propagation and micro-thrust calibration for small satellites
[J]. Chinese Space Science and Technology, 2022, 42(2): 71-81.
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[2] |
QIN Jiankai, LI Peng.
High-accuracy target tracking estimation based on dual Kalman filter
[J]. Chinese Space Science and Technology, 2021, 41(5): 116-124.
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[3] |
QI Hangtian, ZHANG Xiaolin, ZHU Lijin.
Carrier loop for high dynamic and weak signal in deep space#br#
[J]. Chinese Space Science and Technology, 2020, 40(1): 19-.
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[4] |
KANG Guohua, FAN Kai, ZHOU Qiongfeng, LIANG Ertao.
Attitude determination algorithmfor micro-satellite based on Gauss-Newton and UKF
[J]. Chinese Space Science and Technology, 2018, 38(2): 16-23.
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[5] |
SHI Heng, XU Shi-Jie.
Autonomous Navigation and In-orbit Parameter Calibration for Continuous Low Thrust Spacecraft
[J]. Chinese Space Science and Technology, 2012, 32(4): 62-70.
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[6] |
YUE Xiao-Kui, LI Bin, ZHAO Kai.
Vision-based IMM-UKF Spacecraft Relative Position and Attitude Determination Algorithm
[J]. Chinese Space Science and Technology, 2012, 32(3): 7-14.
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[7] |
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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[8] |
LIU Wen-Xiang, MOU Wei-Hua, WANG Fei-Xue.
Effect Analysis of Measuring Time Error on Single Satellite Orbit Determination Error
[J]. Chinese Space Science and Technology, 2011, 31(4): 70-76.
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[9] |
ZHANG Bao-Qun, SONG Shen-Min, CHEN Xing-Lin.
Decentralized Attitude Coordination Control of Satellites within Formation under Input Constraints
[J]. Chinese Space Science and Technology, 2011, 31(1): 16-24.
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[10] |
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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[11] |
Hu Min Zeng Guoqiang Yao Hong Li Xiaoming (Academy of Equipment Command & Technology,Beijing 101416).
Safety for Near Round Reference Orbit Satellites Formation
[J]. Chinese Space Science and Technology, 2010, 30(04): 16-22.
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[12] |
Han Lu Jing Zhanrong Li Dong Duan Zhemin (School of Electronic&Information,Northwestern Polytechnical University,Xi′an 710072).
Attitude Independent GPS Ambiguity Resolution Using UKF
[J]. Chinese Space Science and Technology, 2010, 30(03): 31-36.
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[13] |
Fan Chunshi1 Zhang Gaofei2 Sun Jian2 Meng Ziyang1 You Zheng1(1 Department of Precision Instruments and Mechanology,Tsinghua University,Beijing 100084)(2 State Key Laboratory of Precision Measurement Technology and Instruments,Tsinghua University,Beijing 100084).
Federated SSUKF for Multi-sensor Spacecraft Attitude Estimation
[J]. Chinese Space Science and Technology, 2009, 29(06): 21-27+80.
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[14] |
Wang Hui Gu Xuemai(Harbin Institute of Technology,Harbin 150001).
Autonomous Determination of Relative Orbit for Satellite Formation Flying Using Radio-only Measurement
[J]. Chinese Space Science and Technology, 2009, 29(04): 37-45.
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[15] |
Li Yang1 Zhang Running2(1 Institution of Communication Satellite,China Academy of Space Technology,Beijing 100094)(2 Dong Fang Hong Satellite Co.Ltd,Beijing 100094).
Orbit Configuration Design and Perturbation Analysis Based on Formation Flying InSAR Satellites Mission and Performance Requirements
[J]. Chinese Space Science and Technology, 2009, 29(04): 46-53.
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