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GPS-correction in the problem of low-orbit spacecraft navigation

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Abstract

Algorithms for the spacecraft navigation with correction by messages of a global positioning satellite system are proposed. This approach to solving the navigation problem allows for the combination of a given average level of accuracy with saving of computation resources.

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Authors and Affiliations

  1. International Research and Training Center for Information Technologies and Systems, National Academy of Sciences of Ukraine, pr. akademika Glushkova 40, Kiev, 03680, Ukraine

    A. I. Tkachenko

Authors
  1. A. I. Tkachenko
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Original Russian Text © A.I. Tkachenko, 2009, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2009, No. 3, pp. 122–133.

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Tkachenko, A.I. GPS-correction in the problem of low-orbit spacecraft navigation. J. Comput. Syst. Sci. Int. 48, 447–457 (2009). https://doi.org/10.1134/S1064230709030113

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  • DOI: https://doi.org/10.1134/S1064230709030113

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