Construction of the initial deorbit region for landing at the given place
- Авторы: 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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Учреждения:
- Keldysh Institute of Applied Mathematics
- Korolev Rocket and Space Corporation Energia
- Выпуск: Том 56, № 2 (2017)
- Страницы: 300-310
- Раздел: 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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Аннотация
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.
Об авторах
S. Evdokimov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
S. Klimanov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Автор, ответственный за переписку.
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
A. Korchagin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
E. Mikrin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
Yu. Sikharulidze
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
A. Tuchin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Россия, Moscow; Moscow
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