[1] |
YANG Kaifei, HAN Xiaodong, LYU Yuancao, XU Nan, GONG Jianglei, LI Xiang.
Satellite fault detection method based on time-series modeling
[J]. Chinese Space Science and Technology, 2023, 43(2): 93-102.
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[2] |
WU Kongyang, YE Xiaozhou, XIAO Wei, LIU Wenxiang, LIU Xiaohui.
An autonomous integrity monitoring method of integrated navigation based on multiple virtual observations #br#
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[J]. Chinese Space Science and Technology, 2021, 41(3): 60-69.
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[3] |
PENG Zhen, JIN Xiaojun, MO Shiming, ZHANG Wei, XU Zhaobin, JIN Zhonghe.
Real-time calibration method for groundbased TT&C systems using satellite-to-ground differential GPS
[J]. Chinese Space Science and Technology, 2020, 40(6): 77-88.
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[4] |
YE Zipeng, ZHOU Qingrui, WANG Hui.
Research on autonomous navigation method for deep space exploration spacecraft in cruise phase
[J]. Chinese Space Science and Technology, 2020, 40(5): 53-60.
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[5] |
XU Xiaohan, WANG Kedong.
Online design of optimal carrier tracking loop bandwidth for tightlycoupled GPS/INS
[J]. Chinese Space Science and Technology, 2019, 39(2): 49-57.
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[6] |
CHEN Xin, WEI Bingyi, WEN Xin.
Study of support vector machine based faults diagnosis for satellite′s actuators
[J]. Chinese Space Science and Technology, 2018, 38(2): 47-55.
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[7] |
ZHANG Jian-Li, YANG Zu-Fang, PAN Wei, ZHENG Jian-Sheng.
DesignandimplementationofinterferencesuppressionalgorithmforBeiDouandGPSdual-frequencyreceiver
[J]. Chinese Space Science and Technology, 2017, 37(1): 117-123.
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[8] |
LEI Yu, LI Bian, ZHAO Dan-Ning, HU Yong-Hui.
RealtimePredictionAlgorithmforHighaccuracyGPSSatelliteClockOffset
[J]. Chinese Space Science and Technology, 2014, 34(4): 38-.
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[9] |
IN Ning, QIU Le-de ZHANG Li-hua, DING Yan-wei.
An On-orbit Calibration Method of KBR Phase Center
[J]. Chinese Space Science and Technology, 2014, 34(1): 50-56.
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[10] |
LIU Wei-Xia, XIONG Zhi, YU Feng, YAO Xiao-Song.
On-orbit Calibration Technique Based on the Two-step Moment of Inertia Identification of the Combination Spacecraft
[J]. Chinese Space Science and Technology, 2013, 33(2): 32-40.
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[11] |
WANG Zheng, LI Yan-Jun, SUN Xiao-Wei.
High Precision Nonlinear FDD Design Using RBF with the Ability to Learn
[J]. Chinese Space Science and Technology, 2012, 32(1): 27-35.
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[12] |
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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[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] |
Wang Lifeng Yang Hui Wang Jingang(China Academy of Space Technology,Beijing 100094).
Study of Fault Detection Method for 3+1S Gyro Unit
[J]. Chinese Space Science and Technology, 2009, 29(06): 52-58.
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[15] |
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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