69520

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Доклад

Название: 

Optimization of the interplanetary flight to Mars with three-pulse approach to Phobos based on Lagrange principle

Электронная публикация: 

Да

ISBN/ISSN: 

1742-6596

DOI: 

10.1088/1742-6596/1864/1/012130

Наименование конференции: 

  • 13th Multiconference on Control Problems (MCCP 2020), Saint-Petersburg

Наименование источника: 

  • Journal of Physics: Conference Series

Обозначение и номер тома: 

vol. 1864, № 1

Город: 

  • Bristol, UK, England

Издательство: 

  • IOP Publishing

Год издания: 

2021

Страницы: 

https://iopscience.iop.org/article/10.1088/1742-6596/1864/1/012130/meta
Аннотация
The problem of optimal control of the spacecraft interplanetary flight from the Earth to Mars with a three-pulse approach to the Phobos tracking orbit is considered. The departure of the spacecraft from the Earth is also approximated by pulses. The attraction of the Earth and Mars is taken into account. The problem is solved numerically on the basis of Lagrange principle. The results are compared with the scheme of a full turn free approach to Phobos. The initial approximation is carried out based on a combination of Lambert problems solutions. The software package is developed. Ephemerides are taken into account in the calculations, and the NASA SPICE package is used.

Библиографическая ссылка: 

Самохин А.С., Самохина М.А. Optimization of the interplanetary flight to Mars with three-pulse approach to Phobos based on Lagrange principle / Journal of Physics: Conference Series. Bristol, UK, England: IOP Publishing, 2021. vol. 1864, № 1. С. https://iopscience.iop.org/article/10.1088/1742-6596/1864/1/012130/meta.