Volume 43 Issue 3
Jul.  2023
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DUAN Jianfeng, ZHANG Yu, KONG Jing, CHEN Ming, LI Cuilan. Evaluation of Orbit Determination Accuracy in Interplanetary Transfer Section of Mars Probe (in Chinese). Chinese Journal of Space Science, 2023, 43(3): 499-506 doi: 10.11728/cjss2023.03.2022-0008
Citation: DUAN Jianfeng, ZHANG Yu, KONG Jing, CHEN Ming, LI Cuilan. Evaluation of Orbit Determination Accuracy in Interplanetary Transfer Section of Mars Probe (in Chinese). Chinese Journal of Space Science, 2023, 43(3): 499-506 doi: 10.11728/cjss2023.03.2022-0008

Evaluation of Orbit Determination Accuracy in Interplanetary Transfer Section of Mars Probe

doi: 10.11728/cjss2023.03.2022-0008 cstr: 32142.14.cjss2023.03.2022-0008
  • Received Date: 2022-04-18
  • Rev Recd Date: 2022-07-23
  • Available Online: 2023-02-14
  • Tianwen-1 is the first Chinese probe to realize interplanetary flight between Earth and Mars. During the 202-day long interplanetary transfer flight, it experienced four midway corrections and one deep space maneuver control. On 10 February 2021, it successfully applied braking near Mars and was captured by Mars. This paper, the dynamic model during interplanetary transfer is analyzed, and the principle of celestial center conversion during transfer flight is formulated. It is necessary to replace the celestial center with the Sun after leaving the Earth’s influence sphere. According to the analysis results, DE436 ephemeris is determined to be used, because it has the least impact on orbit determination. Based on the characteristics of the interplanetary transfer flight of the probe, this paper proposes an accuracy evaluation method based on a daily iterative orbit determination strategy. Based on the analysis of measured data, the effectiveness of this method has been verified. During the interplanetary transfer of the Mars probe, the orbit determination position error is better than 2 km, and the velocity error is better than mm·s–1 (1σ).

     

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