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《JOURNAL OF ASTRONAUTICS》 1994-02
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METHOD OF MEASUREMENT IN THE STAGE OF FINAL APPROACHING FOR RENDEZVOUS AND DOCKING IN SPACE

Lin Laixing; Li Can(Beijing Institute of Control Engineering)  
This paper offers two measurement schemes for CCD camera in the stage of final approaching of RVD,no matter how the attitude and position of CCDS are installed.For one or more than one cameras,the algorithms are not the same. The algorithm based upon two or more cameras is fairly easy and fast,and the one based upon one camera is possibly more accurate. Combination of two means can deal well with the problem of measurement in the stage of final approaching.
【CateGory Index】: V526
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1 LI Peng~(1,2),DUAN Guangren~2,SONG Shenmin~2 1.Xiangtan University,College of Information and Technology,Xiangtan 411105,P.R.China 2.Harbin Institute of Technology,Harbin 150001,P.R.China;Design of Relative Measurement System for Docking and Separation Platform Based on MIMU/CCD[A];[C];2011
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8 JIANG Gang-wu,GONG Hui,WANG Jing,JIANG Ting(Institute of Surveying and Mapping,Information Engineering University,Zhengzhou 450052,China);The Optical Measurement of Self-Calibration in Orbit for Spacecraft Rendezvous and Docking[J];宇航学报;2007-01
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【Co-references】
Chinese Journal Full-text Database 10 Hits
1 SONG Liang;LI Zhi;MA Xing-rui;Qian Xuesen Laboratory of Space Technology,China Academy of Space Technology;Government of Guangdong Province;;A Novel Position and Attitude Estimation for Space Debris[J];宇航学报;2015-08
2 ZHAI Kun;QU Xi;LI Zhi;CHEN Xinlong;School of Astronautics and Aerospace,Tsinghua University;Institute of Manned Space System Engineering,China Academy of Space Technology;Qian Xuesen Laboratory of Space Technology,China Academy of Space Technology;;Ground test and relative attitude determination algorithms of non-cooperative spacecraft[J];哈尔滨工业大学学报;2014-03
3 XU Pei-zhi,XU Gui-li,WANG Biao,GUO Rui-peng,TIAN Yu-peng,YE Yong-qiang(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);Pose Measurement of Non-Cooperative Target Based on Stereo Vision[J];计算机与现代化;2013-08
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5 Li Jing1 Wang Huinan2 Liu Haiying3(1 College of Automation Engineering,Nanjing University of Aerospace and Astronautics,Nanjing 210016)(2 College of Astronautics,NUAA,Nanjing 210016)(3 Academy of Frontier Science,NUAA,Nanjing 210016);Plucker Linear Based Relative Position and Attitude Determination Algorithm for RVD[J];中国空间科学技术;2013-01
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7 QIAN Ping,WANG Hui-nan(College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);A Binocular Vision Algorithm Based on Dual Quaternion for Relative Position and Attitude Determination of RVD Spacecrafts[J];宇航学报;2013-01
8 ZHAI Guang1,2,ZHANG Jing-rui2,ZHOU Zhi-cheng3(1.Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education,Beijing 100081,China; 2.School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China; 3.China Academy of Space Technology,Beijing 100094,China);A Review of On-Orbit Life-Time Extension Technologies for GEO Satellites[J];宇航学报;2012-07
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10 LIANG Bin~1,DU Xiaodong~1,LI Cheng~1,XU Wenfu~2 (1.The Institute of Space Intelligent System,Harbin Institute of Technology,Harbin 150001,China; 2.Shenzhen Graduate School,Harbin Institute ofTechnology,Shenzhen 518055,China);Advances in Space Robot On-orbit Servicing for Non-cooperative Spacecraft[J];机器人;2012-02
【Secondary References】
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1 ZHAO Lin;ZHANG Guo-qi;Departmentof Automatic,Harbin Engineering University;;Relative Pose Determination Method Based on Genetic Algorithm[J];中小企业管理与科技(中旬刊);2017-06
2 FENG Jigen;GUO Jifeng;College of Electrical Engineering, Zhejiang University;;Research of Tether Tension Optimum Control Strategy for Space Tethered-net[J];机械工程师;2017-06
3 LIU Huawei;LIU Yongjian;TAN Chunlin;LIU Yuqiang;Beijing Institute of Spacecraft System Engineering;;Analysis and Suggestion on Key Technology of Space Debris Removal[J];航天器工程;2017-02
4 ZHANG Pin-liang;GONG Zi-zheng;YANG Wu-lin;CHEN Chuan;Beijing Institute of Spacecraft Environment Engineering;;Three-Dimensional Simulation and Modeling on Removing Orbital Debris with Lasers[J];宇航学报;2017-03
5 HE Liyuan;CHEN Zhiming;ZHAO Ping;College of Astronautics,Nanjing University of Aeronautics and Astronautics;;The kinematic modeling based on motor algebra for robotic manipulators[J];机械设计与制造工程;2017-02
6 XU Chenggang;DENG Zhiliang;School of Electrics and Information Engineering,Jiangsu University of Science an Technology;;Research on hand-eye calibration based on mortor algebra[J];江苏科技大学学报(自然科学版);2017-01
7 CHEN Hui-xing;REN Yan;YU Shao-xing;Xichang Satellite Launch Center;State Key Laboratory of NBC Protection;Spaceflight Project Command;;Fuzzy Fault Tree Analysis on Temperature Control System of Conventional Rocket Propellant[J];宇航学报;2017-01
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10 PANG Zhenan;ZHANG Guoliang;YANG Fan;JIA Xiao;LIN Zhilin;Department of Control Engineering,Rocket Force University of Engineering;Baoji New High Tech Research Institute;;Adaptive tracking control and vibration suppression by fuzzy neural network for free-floating flexible space robot with limited torque[J];计算机应用;2016-10
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1 HUANG Yuming (Institute 502,Ministry of Aerospace,Beijing 100080)YANG Shiqiang XU Guangyou (Computer Science Department,Qinghua University,Beijing 100084) The modern industrial color camera is mainly used as an input equipment for image monitor,and itsperformence standard is the image quality percepted by human vision.It does not meet the demand of col-or sensor in computer vision system completely;therefore,measurement and calibration of the camera arenecessary.This paper describes a method for restoring the spectral linearility of color CCD camera.Exper-iment shows that the effect of light intensity to color Coordinate can be removed or lightened.The imageafter transform looks just a bit darker than the original one.At last,application of this method to colormeasurement is presented.Results show that the accuracy of color measurement using color CCD camerais improved.;SPECTRAL LINEARIZATION OF COLOR CCD CAMERA AND ITS APPLICATION IN COLOR MEASUREMENT[J];机器人;1992-01
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