Refinement of the Orbit of the Space Radio Telescope in the Millimetron (Spektr-M) Project
П. Р. Запевалин, A. G. Rudnitskiy, М. А. Щуров, T. A. Syachina
Abstract
П. Р. Запевалин, A. G. Rudnitskiy, М. А. Щуров, T. A. Syachina
Abstract
As part of the creation of the Millimetron Space Observatory, the task was set to develop a reliable tool for ballistic and navigational support of the Spektr-M spacecraft. This article describes software developed to determine and refine the orbital parameters of spacecraft, including the Millimetron Observatory. This paper briefly describes the project of the Spektr-M observatory, algorithms for determining the orbit, and presents the results of the software. In addition, the number of ground-based tracking stations was estimated for optimal measurements of the orbit of the Spektr-M spacecraft to ensure the required orbital accuracy and to reduce the time the space observatory is out of sight. The implemented algorithms were tested on model and real observation data.
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As part of the creation of the Millimetron Space Observatory, the task was set to develop a reliable tool for ballistic and navigational support of the Spektr-M spacecraft. This article describes software developed to determine and refine the orbital parameters of spacecraft, including the Millimetron Observatory. This paper briefly describes the project of the Spektr-M observatory, algorithms for determining the orbit, and presents the results of the software. In addition, the number of ground-based tracking stations was estimated for optimal measurements of the orbit of the Spektr-M spacecraft to ensure the required orbital accuracy and to reduce the time the space observatory is out of sight. The implemented algorithms were tested on model and real observation data.
Key concepts: Spacecraft, Observatory, Orbit determination, Orbital mechanics, Orbit (dynamics), Software, Computer science, Physics