2014
DOI: 10.1134/s0010952514050128
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Navigation support for the RadioAstron mission

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Cited by 13 publications
(8 citation statements)
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“…The satellite telemetry and science data are received and recorded at tracking stations in Puschino (Andreyanov et al 2014) and Green Bank (Ford et al 2014) and later transferred for correlation at one of the RadioAstron correlation facilities. Accurate reconstruction of the orbit and of the momentary state vector of the Spektr-R spacecraft is achieved by combining together radiometric range and radial velocity measurements made at the satellite control stations in Bear Lakes and Ussurijsk (Russia), Doppler measurements obtained at each of the tracking stations, and laser ranging and optical astrometric measurements of the spacecraft position in the sky Zakhvatkin et al 2014). The accuracy can be further enhanced by simultaneous VLBI measurements performed on the narrow-band downlink signal from the spacecraft (Duev et al 2012).…”
Section: Imaging With Radioastronmentioning
confidence: 99%
“…The satellite telemetry and science data are received and recorded at tracking stations in Puschino (Andreyanov et al 2014) and Green Bank (Ford et al 2014) and later transferred for correlation at one of the RadioAstron correlation facilities. Accurate reconstruction of the orbit and of the momentary state vector of the Spektr-R spacecraft is achieved by combining together radiometric range and radial velocity measurements made at the satellite control stations in Bear Lakes and Ussurijsk (Russia), Doppler measurements obtained at each of the tracking stations, and laser ranging and optical astrometric measurements of the spacecraft position in the sky Zakhvatkin et al 2014). The accuracy can be further enhanced by simultaneous VLBI measurements performed on the narrow-band downlink signal from the spacecraft (Duev et al 2012).…”
Section: Imaging With Radioastronmentioning
confidence: 99%
“…HALCA and Astro-G used circular near-Earth orbits, providing (u, v) coverage of satisfactory quality for imaging observations [32,33]. Radioastron mission had a high elliptical near-Earth (HEO) orbit with an apogee of ≈ 330,000 km, which made it possible to achieve the highest angular resolution of 8 µas at the shortest wavelength of the mission (λ = 1.3 cm) [34,35].…”
Section: Orbital Configurationsmentioning
confidence: 99%
“…To look for a possible violation using measured fractional frequency shifts, the state parameters for the spacecraft must be known with sufficient accuracy to isolate the gravitational redshift from other effects, particularly the much larger non-relativistic Doppler effect. Orbit determination for the RadioAstron mission is done using a variety of sources of data, among them the same frequency observations made at the PU and GB ground stations 6 used in this analysis (Zakhvatkin et al, 2013(Zakhvatkin et al, , 2018. The position and velocity of the spacecraft are determined using a least-squares minimization in which no violation is assumed.…”
Section: Feasibility Of Determining the Violation Parametermentioning
confidence: 99%