Volume 38 Issue 6
Nov.  2018
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Article Navigation >  Chinese Journal of Space Science  > 2018  >  38(6): 915-924
LI Lan, LI Changgeng, HUANG Wende, ZHOU Yifan. Orbit Determined Method of High Elliptical Orbit Satellite Based on BDS Navigation and Inter-satellite Link[J]. Chinese Journal of Space Science, 2018, 38(6): 915-924. doi: 10.11728/cjss2018.06.915
Citation: LI Lan, LI Changgeng, HUANG Wende, ZHOU Yifan. Orbit Determined Method of High Elliptical Orbit Satellite Based on BDS Navigation and Inter-satellite Link[J]. Chinese Journal of Space Science, 2018, 38(6): 915-924. doi: 10.11728/cjss2018.06.915
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Orbit Determined Method of High Elliptical Orbit Satellite Based on BDS Navigation and Inter-satellite Link

doi: 10.11728/cjss2018.06.915 cstr: 32142.14.cjss2018.06.915

  • 1. School of Physics and Electronics, Central South University, Changsha 410000;

  • 2. College of Mechanical Engineering and Automation, National University of Defense Technology, Changsha 410073

  • Received Date: 2017-10-31
  • Rev Recd Date: 2018-04-16
  • Publish Date: 2018-11-15
    Abstract
  • The traditional ground tracking telemetry control and Global Navigation Satellite System (GNSS) are unable to achieve the whole orbit observation of the High Elliptical Orbit (HEO). An autonomous navigation method is put forward, which combines the satellite navigation and inter-satellite link. This method is based on the Beidou Navigation Satellite System (BDS) navigation and inter-satellite link complementary characteristics of HEO monitoring after analyzing the observation geometry and the coverage characteristics of the typical HEO track. The autonomous navigation algorithm is designed for orbit determination, which combines the satellite navigation and inter-satellite link data based on Extended Kalman Filter (EKF). The HEO satellite orbit determination is divided into some segments. The analysis results show that the proposed method can improve the HEO satellites' observation geometry for the whole orbit, and the orbit prediction precision is enhanced by over two orders of magnitude compared with the BDS navigation method. Furthermore, the occupation of the inter-satellite link resources decreases significantly.

     

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