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Autonomous optical navigation for interplanetary exploration based on information of earth-moon 被引量:2

Autonomous optical navigation for interplanetary exploration based on information of earth-moon
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摘要 The image elements of earth-center and moon-center are obtained by processing the images of earthand moon, these image elements in combination with the inertial attitude information and the moon ephemerisare utilized to obtain the probe initial position relative to earth, and the Levenberg-Marquardt algorithm is usedto determine the accurate probe position relative to earth, and the probe orbit relative to earth is estimated by u-sing the extended Kalman filter. The autonomous optical navigation algorithm is validated using the digital simu-lation. The image elements of earth-center and moon-center are obtained by processing the images of earth and moon, these image elements in combination with the inertial attitude information and the moon ephemeris are utilized to obtain the probe initial position relative to earth, and the Levenberg-Marquardt algorithm is used to determine the accurate probe position relative to earth, and the probe orbit relative to earth is estimated by using the extended Kalman filter. The autonomous optical navigation algorithm is validated using the digital simulation.
出处 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2003年第3期343-348,共6页 哈尔滨工业大学学报(英文版)
关键词 行星探测器 自主光学导航 数字仿真 图像处理 像素 地球 月球 扩展卡尔曼滤波器 autonomous optical navigation interplanetary exploration Levenberg-Marquardt algorithm
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参考文献11

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二级参考文献19

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共引文献7

同被引文献18

  • 1徐文明,崔祜涛,崔平远,刘宇飞.深空自主光学导航小行星筛选与规划方法研究[J].航空学报,2007,28(4):891-896. 被引量:9
  • 2Desai S,Han D,Bhaskaran S,et al.Autonomous optical navigation (autoNav) technology validation report[J].Deep Space 1 Technology Validation Report-Autonomous Optical Navigation (AutoNav),2002:1-39.
  • 3Nikos Mastrodemos,Daniel G,Kubitschek,Robert A,Werner,et al.Autonomous navigation for the deep impact[C]// Proceedings of the AAS/AIAA Space Flight Mechanics Meeting:Tampa,Florida,January 22-26 2006:1251-1271.
  • 4Marini A E,Racca G D,Foing B H.SMART-1 technology preparation for future planetary missions[J].Advaces in Space Research,2002,30(8):1895-1900.
  • 5Kubota T,Hashimoto T,Kawaguchi J,Sawai S,et al.Navigation,guidance and control of asteroid sample return spacecraft:MUSES-C[C]// Proceedings 4th ESA International Conference on Spacecraft Guidance,Navigation and Control Systems,ESTEC,Noordwijk,Netherlands,October 18-21,1999.ESA SP-425 2000:511-516.
  • 6Bhaskaran S,Desai D,Dumont P J,et al.Orbit determination performance evaluation of the deep space 1 autonomous navigation system[C]// Proceedings of the AAS/AIAA Spaceflight Mechanics Meeting,Monterrey,CA,Feb.9-12,1998,AAS 98-193:1295-1314.
  • 7Guo Y P.Self-contained autonomous navigation system for deep space missions[J].Advances in the Astronautical Sciences,1999,102(2):1099-1113.
  • 8Bhaskaran S,Riedel J E,Synnott S P.Autonomous nucleus tracking for comet/asteroid encounters:the STARDUST example.1998 IEEE Aerospace Conference,Aspen,CO,Mar.21-28,1998.Proceedings,Piscataway,NJ,Institute of Electrical and Electronics Engineers,1998,2:353-365.
  • 9William H,Blume.Deep impact mission design[J].Space Science Reviews,2005,117:23-42.
  • 10DESAI S,HAN D,BHASKARAN S.et al.Autonomous optical navigation (AutoNav) technology validation report[R].Deep Space 1 Technology Validation Report-Autonomous Optical Navigation (AutoNav),JPL Publication 00-10,2000.

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