2015
DOI: 10.1051/0004-6361/201424940
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RadioAstron as a target and as an instrument: Enhancing the Space VLBI mission’s scientific output

Abstract: Context. The accuracy of orbit determination has a strong impact on the scientific output of the Space VLBI mission RadioAstron. Aims. The aim of this work is to improve the RadioAstron orbit reconstruction by means of sophisticated dynamical modelling of its motion in combination with multi-station Doppler tracking of the RadioAstron spacecraft. Methods. The improved orbital solution is demonstrated using Doppler measurements of the RadioAstron downlink signal and by correlating VLBI observations made by Radi… Show more

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Cited by 15 publications
(15 citation statements)
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“…2. These slowly evolving residuals agree well with the expected accuracy of the orbital velocity determination for the SRT (Kardashev et al 2013), but they still should be viewed only as an indicator of the fidelity of the fringe fitted data, while a more detailed discussion of the accuracy of the orbit determination for the SRT is presented elsewhere (Duev et al 2015).…”
Section: Fringe Fittingsupporting
confidence: 76%
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“…2. These slowly evolving residuals agree well with the expected accuracy of the orbital velocity determination for the SRT (Kardashev et al 2013), but they still should be viewed only as an indicator of the fidelity of the fringe fitted data, while a more detailed discussion of the accuracy of the orbit determination for the SRT is presented elsewhere (Duev et al 2015).…”
Section: Fringe Fittingsupporting
confidence: 76%
“…The accuracy can be further enhanced by simultaneous VLBI measurements performed on the narrow-band downlink signal from the spacecraft (Duev et al 2012). This was demonstrated (Duev et al 2015) using the data from the ESP observations of 0642+449 discussed here.…”
Section: Imaging With Radioastronmentioning
confidence: 85%
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“…The solutions are consistent between the two IF bands, and the likely effect of the satellite acceleration is reflected both in the time variations of the fringe delays and in the respective delay rates. The overall behavior of the fringe solutions is in agreement with the expected accuracy of the orbital position and velocity determination (Kardashev et al 2013;Duev et al 2015;Lobanov et al 2015).…”
Section: Fringe Fittingsupporting
confidence: 79%
“…In the EHI concept we consider a different approach in which the baseline vector and its time derivatives are obtained (measured) directly between the EHI spacecraft in real time. As demonstrated by RadioAstron, orbit determination measurements (not to confuse with orbit reconstruction) are provided by means of radio measurements at the level that correspond to ∼ 20 to 1500 observing wavelengths at 92 to 1.3 cm, respectively, and radial velocity (Doppler) measurements at the mm/s accuracy level (Zakhvatkin et al 2014;Duev et al 2015). Escalating similar requirements for the EHI sub-mm wavelength range leads to the baseline measurement re-quirements at a precision level of ∼ 20 cm for the baseline vector and 0.01 mm/s for its time derivative.…”
Section: Martinmentioning
confidence: 99%