Orbit determination by cued observation using correlator radio telescope arrays: System model and performance evaluation

We study repurposing radio astronomy correlator arrays for orbit refinement of resident space objects RSOs in the context of space situational awareness (SSA). By developing a suitable near-field interferometry signal model, we derive a 3D multiple signal classification (MUSIC) estimator to estimate...

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Bibliographic Details
Published inActa astronautica Vol. 236; pp. 503 - 513
Main Authors Nosrati, Ryan (Hamed), Biswas, Sanat, Smith, Stephanie, Hayman, Douglas B.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.11.2025
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ISSN0094-5765
DOI10.1016/j.actaastro.2025.06.011

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Summary:We study repurposing radio astronomy correlator arrays for orbit refinement of resident space objects RSOs in the context of space situational awareness (SSA). By developing a suitable near-field interferometry signal model, we derive a 3D multiple signal classification (MUSIC) estimator to estimate the right ascension (RA), declination (Dec), and range offsets, allowing for the refinement of the position vector. This refined position vector is then utilized in an extended Kalman filter (EKF) to determine the new orbit, leading to improved accuracy and precision. Drawing inspiration from the configuration of the Australia Telescope Compact Array (ATCA) and correlator, we develop an observation simulator to produce measurement vectors for observation scenarios of perturbed trajectories at geostationary orbit (GEO), medium earth orbit (MEO), and low-earth orbit (LEO) regimes. We apply the proposed system model and demonstrate that the state estimation error is significantly reduced, leading to more accurate orbit refinement. Furthermore, our experimental results for radio observations made by ATCA provide further evidence for the effectiveness of the proposed strategy. •Radio telescopes track resident space objects to contribute to situational awareness•New method determines satellite direction and range to refine orbital elements•Method proven effective across various orbital regimes and validated on real data.
ISSN:0094-5765
DOI:10.1016/j.actaastro.2025.06.011