Construction of the initial deorbit region for landing at the given place
- Авторлар: 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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Мекемелер:
- Keldysh Institute of Applied Mathematics
- Korolev Rocket and Space Corporation Energia
- Шығарылым: Том 56, № 2 (2017)
- Беттер: 300-310
- Бөлім: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219861
- DOI: https://doi.org/10.1134/S106423071702006X
- ID: 219861
Дәйексөз келтіру
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.
Авторлар туралы
S. Evdokimov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
S. Klimanov
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Хат алмасуға жауапты Автор.
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
A. Korchagin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
E. Mikrin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
Yu. Sikharulidze
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
A. Tuchin
Keldysh Institute of Applied Mathematics; Korolev Rocket and Space Corporation Energia
Email: sikh@kiam1.rssi.ru
Ресей, Moscow; Moscow
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