Volume 44 Issue 10
Oct.  2019
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HAO Wanhong, LU Mingquan. Phase Estimation for Inter-agency Interferometric Tracking in Chang'E-3 Powered Descent Flight[J]. Geomatics and Information Science of Wuhan University, 2019, 44(10): 1442-1448. DOI: 10.13203/j.whugis20180020
Citation: HAO Wanhong, LU Mingquan. Phase Estimation for Inter-agency Interferometric Tracking in Chang'E-3 Powered Descent Flight[J]. Geomatics and Information Science of Wuhan University, 2019, 44(10): 1442-1448. DOI: 10.13203/j.whugis20180020
shu

Phase Estimation for Inter-agency Interferometric Tracking in Chang'E-3 Powered Descent Flight

  • 1.

    Department of Electronic Engineering, Tsinghua University, Beijing 100084, China

  • 2.

    Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China

Funds: Chinese Lunar Exploration Program
More Information
  • Author Bio:

    HAO Wanhong, PhD, specializes in deep space radio-metric tracking and signal processing techniques. E-mail:haowanhong@bittt.cn

  • Corresponding author:

    LU Mingquan, PhD, professor. E-mail: lumq@tsinghua.edu.cn

  • Received Date: July 03, 2018
  • Published Date: October 04, 2019
    Graphical Abstract
    • Abstract
  • Very long baseline interferometry plays a critical role on the orbit determination of the lunar and deep space probes, as well as the radio science research. Based on a first-order approximation model of the probe's topocentric range-rate, this paper proposes a new narrow band tracking method for the weak signal received by an antenna with relatively small aperture. As long as the Doppler dynamics has been estimated from the signal received by a large antenna with high G/T value, the weak signal, received by the small antenna during the same time duration, could be Doppler compensated. The raw data acquired by Chinese Jiamusi station and European Space Agency's New Norcia station have been processed, and the results demonstrate the effectiveness of this method. Digital phase locked loop with 5 Hz noise bandwidth could be used to track the differential one-way ranging(DOR) tone received by New Norcia, after Doppler compensation by estimation results from Jiamusi carrier tracking, and the root mean square of the tracking phase errors for DOR tone is around 3.4 degree. This method could be used in the radio metric navigation for the future lunar and deep space missions, as well as the inter-agency cross-supports.
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    • References (11)
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