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SATELLITES: 作品数：298被引量：600H指数：13; 导出分析报告; 相关领域：航空宇航科学技术电子电信更多>>; 相关作者：杨军许健民董超华贾朔孙楫舟更多>>; 相关机构：中国电子技术标准化研究院南京航空航天大学中国电子科技集团第二十九研究所国家卫星气象中心更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划国家高技术研究发展计划中国博士后科学基金更多>>

Two-phase visual servoing for capturing tumbling non-cooperative satellites with a space manipulator: 《Chinese Journal of Aeronautics》2024年第12期560-573,共14页Dezhi ZHANG Guocai YANG Yongjun SUN Junhong JI Minghe JIN Hong LIU; supported by the China Postdoctoral Science Foundation(No.2022M710956).; In this paper,a visual servoing approach is developed to capture the docking rings of tumbling non-cooperative satellites with a space manipulator.The primary challenge addressed is the potential for the docking ring ...; 关键词：Space manipulator Tumbling non-cooperative satellite Visual servoing Model predictive control Disturbance estimation

Payload-oriented control scheme for rotating payload satellite considering inertia uncertainties and measurement errors: 《Chinese Journal of Aeronautics》2023年第10期335-352,共18页Yatao ZHAO Cheng WEI Chengfei YUE Xibin CAO; the Open Fund of Heilongjiang Postdoctoral Fund,China(No.LBH-Z21141).; For the remote sensing satellite with an unbalanced rotating payload suspended by an Active Magnetic Bearing(AMB),this paper proposes a payload-oriented control scheme where the high-precision payload attitude control...; 关键词：Attitude control Identification Payload-oriented scheme SATELLITES State estimation

Precise orbit determination for TH02-02 satellites based on BDS3 and GPS observations被引量：2: 《Chinese Journal of Aeronautics》2023年第5期475-485,共11页Houzhe ZHANG Bing JU Defeng GU Ying LIU Kai SHAO Xiaojun DUAN Zhiyong HUANG; funded by the National Natural Science Foundation of China(Nos.61803018 and 41874028);the Key Laboratory Found,China(No.6142210200105);the National Key R&D Program of China(No.2020YFA0713502).; The Tianhui-202(TH02-02)satellite formation,as a supplement to the microwave mapping satellite system Tianhui-201(TH02-01),is the first Interferometric Synthetic Aperture Radar(InSAR)satellite formation-flying system ...; 关键词：BDS3 Multi-GNSS Precise orbit determination Spaceborne GNSS receiver TH02-02

Three-line structured light vision system for non-cooperative satellites in proximity operations被引量：4: 《Chinese Journal of Aeronautics》2020年第5期1494-1504,共11页Yang LIU Zongwu XIE Hong LIU; financial support provided by the Foundation for Innovative Research Groups of the National Natural Science Foundation of China (Nos. 51521003 and 61690210); Adapter ring is a commonly used component in non-cooperative satellites,which has high strength and is suitable to be recognized and grasped by the space manipulator.During proximity operations,this circle feature may...; 关键词：Adapter ring Line detection Non-cooperative target Pose measurement Space robot Structured light

Online scheduling of image satellites based on neural networks and deep reinforcement learning被引量：23: 《Chinese Journal of Aeronautics》2019年第4期1011-1019,共9页Haijiao WANG Zhen YANG Wugen ZHOU Dalin LI; co-supported by the Key Programs of the Chinese Academy of Sciences (No. ZDRW-KT-2016-2);the National High-tech Research and Development Program of China (No. 2015AA7013040); In the ‘‘Internet Plus" era, space-based information services require effective and fast image satellite scheduling. Most existing studies consider image satellite scheduling to be an optimization problem to solve w...; 关键词：DEEP REINFORCEMENT learning Dynamic SCHEDULING IMAGE SATELLITES Neural network Online SCHEDULING

Orbital reference frame estimation with power spectral density constraints for drag-free satellites被引量：1: 《Chinese Journal of Aeronautics》2016年第6期1721-1729,共9页Zhang Yonghe Wang Yamin Mao Qingyun Liang Xuwen; co-supported by the Open Fund of Joint Key Laboratory of Microsatellite of CAS (No. KFKT15SYS1);the Innovation Foundation of CAS (No. CXJJ-14-Q52); The drag-free satellites are widely used in the field of fundamental science as they enable the high-precision measurement in pure gravity fields. This paper investigates the estimation of local orbital reference fram...; 关键词：Drag-free satellite Orbital reference frame Power spectral density State estimation Transfer function

Near minimum-time feedback attitude control with multiple saturation constraints for agile satellites被引量：2: 《Chinese Journal of Aeronautics》2016年第3期722-737,共16页Liu Xiangdong Xin Xing Li Zhen Chen Zhen Sheng Yongzhi; supported by the National Natural Science Foundation of China(Nos.51407011,11372034 and 51207145); Agile satellites are of importance in modern aerospace applications, but high mobility of the satellites may cause them vulnerable to saturation during attitude maneuvers due to limited rating of actuators, This paper...; 关键词：Actuator saturation Attitude control Identification Momentum transfer SATELLITES

Basic performance of BeiDou-2 navigation satellite system used in LEO satellites precise orbit determination被引量：9: 《Chinese Journal of Aeronautics》2014年第5期1251-1258,共8页Liu Junhong Gu Defeng Ju Bing Yao Jing Duan Xiaojun Yi Dongyun; co-supported by the National Natural Science Foundation of China (Nos: 61002033, 61370013);the Program for New Century Excellent Talents in University and the Scientific Research Foundation for the Returned Overseas Chinese Scholars of Ministry of Education of China; The visibility for low earth orbit（LEO） satellites provided by the BeiDou-2 system is analyzed and compared with the global positioning system（GPS）. In addition, the spaceborne receivers＇ observations are simulat...; 关键词：BeiDou-2 Geostationary earth orbit satellites Global positioning system Low earth orbit satellites Precise orbit determination Precise relative orbit determination

Phase Residual Estimations for PCVs of Spaceborne GPS Receiver Antenna and Their Impacts on Precise Orbit Determination of GRACE Satellites被引量：4: 《Chinese Journal of Aeronautics》2012年第4期631-639,共9页TU Jia GU Defeng WU Yi YI Dongyun; National Natural Science Foundation of China(61002033,60902089);Open Research Fund of State Key Laboratory of Astronautic Dynamics of China (2011ADL-DW0103); In-flight phase center systematic errors of global positioning system（GPS） receiver antenna are the main restriction for improving the precision of precise orbit determination using dual-frequency GPS.Residual appro...; 关键词：global positioning system precise orbit determination phase center variations phase residual estimation GRACE

Satellite Constellation Configuration Design with Rapid Performance Calculation and Ordinal Optimization被引量：9: 《Chinese Journal of Aeronautics》2011年第5期631-639,共9页CUI Hongzheng HAN Chao; Satellite constellation configuration design is a complicated and time-consuming simulation optimization problem. In this paper, a new method called the rapid method for satellite constellation performance calculation...; 关键词：SATELLITES rapid performance calculation constellation configuration design ordinal optimization ordered performance curve

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