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Research on autonomous navigation algorithm for spacecraft based on X-ray pulsars

  • Hongliang Yin*
  • , Gongliu Yang
  • , Yanyong Wang
  • , Wenhui Zhang
  • *此作品的通讯作者
  • Beihang University
  • Harbin Institute of Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

An autonomous X-ray pulsars navigation algorithm based on the extended Kalman filter (EKF) is proposed for spacecraft in order to realize 100m position accuracy. The measurement equation of spacecraft position is described with the TOA difference between spacecraft and the solar system barycenter. Then, the EKF, which incorporates spacecraft dynamics and TOA measurements, is developed to estimate spacecraft orbit. Simulation results demonstrate that this navigation algorithm is more accurate as the information contained in the satellite orbit model can be used when the EKF is adopted. 100m position accuracy can be achieved with pulsar orientation errors, 0.001", and timing errors, 0.1μs. Analysis and study show that this method represents high position accuracy, good convergence speed and stability with respect to previous method of least square and maximum likelihood.

源语言英语
主期刊名2011 International Conference on Remote Sensing, Environment and Transportation Engineering, RSETE 2011 - Proceedings
6225-6228
页数4
DOI
出版状态已出版 - 2011
活动2011 International Conference on Remote Sensing, Environment and Transportation Engineering, RSETE 2011 - Nanjing, 中国
期限: 24 6月 201126 6月 2011

出版系列

姓名2011 International Conference on Remote Sensing, Environment and Transportation Engineering, RSETE 2011 - Proceedings

会议

会议2011 International Conference on Remote Sensing, Environment and Transportation Engineering, RSETE 2011
国家/地区中国
Nanjing
时期24/06/1126/06/11

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