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Construction of the initial deorbit region for landing at the given place

  • Control Systems of Moving Objects
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Journal of Computer and Systems Sciences International Aims and scope

Abstract

The algorithm of the two-point boundary problem is developed for choice the nominal deorbit point, from which a descent vehicle is enabled to land at a given place without a cross-range maneuver. The method is suggested and the example is given of constructing the initial deorbit region for landing at the Vostochny cosmodrome.

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References

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Authors and Affiliations

  1. Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russia

    S. N. Evdokimov, S. I. Klimanov, A. N. Korchagin, E. A. Mikrin, Yu. G. Sikharulidze & A. G. Tuchin

  2. Korolev Rocket and Space Corporation Energia, Moscow, Russia

    S. N. Evdokimov, S. I. Klimanov, A. N. Korchagin, E. A. Mikrin, Yu. G. Sikharulidze & A. G. Tuchin

Authors
  1. S. N. Evdokimov
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  2. S. I. Klimanov
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  3. A. N. Korchagin
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  4. E. A. Mikrin
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  5. Yu. G. Sikharulidze
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  6. A. G. Tuchin
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Corresponding author

Correspondence to S. I. Klimanov.

Additional information

Original Russian Text © S.N. Evdokimov, S.I. Klimanov, A.N. Korchagin, E.A. Mikrin, Yu.G. Sikharulidze, A.G. Tuchin, 2017, published in Izvestiya Akademii Nauk, Teoriya i Sistemy Upravleniya, 2017, No. 2, pp. 133–143.

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Evdokimov, S.N., Klimanov, S.I., Korchagin, A.N. et al. Construction of the initial deorbit region for landing at the given place. J. Comput. Syst. Sci. Int. 56, 300–310 (2017). https://doi.org/10.1134/S106423071702006X

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  • DOI: https://doi.org/10.1134/S106423071702006X

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