Simulations Models and Analyses on VLBI Spacecraft Tracking
SUN Jing1, WANG Mei1, PING Jinsong2
Author information+
1. Science and Technology on Aerospace Flight Dynamics Laboratory 2. Key Laboratory of Lunar and DeepSpace Exploration,National Astronomical Observatories
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History+
Received
Revised
25 Jul 2014
17 Aug 2014
Issue Date
20 May 2022
Abstract
Differential VLBI (D-VLBI) is commonly used in VLBI spacecraft tracking in order to reach sufficient accuracy. Despite the simple concept of measuring a spacecraft’s angular distance to a well-known quasar, this method also holds some characteristics that are worth closer inspection. In this paper, the measurement principle is demonstrated and some basic thoughts on the observation sequence and the resultant scan gaps as well as on the separation angle between the reference source and the spacecraft are presented. This is followed by some geometrical reflections on the similarity of the transmission media. The results in this paper will provide technical support for the subsequent spacecraft mission.
SUN Jing, WANG Mei, PING Jinsong.
Simulations Models and Analyses on VLBI Spacecraft Tracking. Journal of Deep Space Exploration, 2014, 1(3): 226‒229 https://doi.org/10.15982/j.issn.2095-7777.2014.03.011
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