Construction of the initial deorbit region for landing at the given place
- Autores: Evdokimov S.1,2, Klimanov S.1,2, Korchagin A.1,2, Mikrin E.1,2, Sikharulidze Y.1,2, Tuchin A.1,2
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Afiliações:
- Keldysh Institute of Applied Mathematics
- Korolev Rocket and Space Corporation Energia
- Edição: Volume 56, Nº 2 (2017)
- Páginas: 300-310
- Seção: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219861
- DOI: https://doi.org/10.1134/S106423071702006X
- ID: 219861
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Resumo
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.
Sobre autores
S. Evdokimov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
S. Klimanov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Autor responsável pela correspondência
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
A. Korchagin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
E. Mikrin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
Yu. Sikharulidze
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
A. Tuchin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Rússia, Moscow; Moscow
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