http://arxiv.org/abs/1812.01623
Orbit determination (OD) is crucial for very-long baseline interferometry (VLBI) experiments conducted with RadioAstron space observatory. The signals recorded by the spacecraft and an Earth-based observatory are to be correlated, which requires accurate delay modeling and thus adequate knowledge of the spacecraft trajectory. In this paper we describe an OD method which was used with the RadioAstron mission in order to achieve orbital accuracy sufficient for successful operation of the ground-space interferometer. In addition to standard ground-based tracking the method utilizes additional information on thrusters firings, rotation of reaction wheels and current attitude of the spacecraft obtained via telemetry channel. The performance of spacecraft navigation for space VLBI experiments with RadioAstron is evaluated in the context of correlation between signals obtained on the Earth and on the orbit, namely residual values found during correlation processing of more than 5000 data scans recorded over 7 years of the mission. Such data contains information about the orbital errors projected on the direction to the observed radio source.
M. Zakhvatkin, A. Andrianov, V. Kostenko, et. al.
Thu, 6 Dec 18
47/52
Comments: 9 pages, 8 figures
You must be logged in to post a comment.