75455

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Доклад

Название: 

On Constructing the Trajectory of Spacecraft Flight to Phobos with a Perturbation Maneuver near the Moon, Based on the Solution of a Combination of 4 Lambert’s Problems

ISBN/ISSN: 

978-5-91995-095-0

DOI: 

10.23919/ICINS51816.2023.10168493

Наименование конференции: 

  • 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS-2023)

Наименование источника: 

  • Proceedings of the 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS-2023)

Город: 

  • Saint Petersburg

Издательство: 

  • IEEE

Год издания: 

2023

Страницы: 

https://ieeexplore.ieee.org/document/10168493
Аннотация
The paper considers the optimization of interplanetary flight to Mars in the impulse statement. The flight schemes with and without perturbation maneuver near the Moon are compared. The trajectories are considered as sets of Lambert's problems and are optimized by gradient methods. Taking into account only one attracting center at each section of the trajectory, the scheme with a maneuver near the Moon allows gaining about 150 m/s in characteristic velocity.

Библиографическая ссылка: 

Самохин А.С., Самохина М.А. On Constructing the Trajectory of Spacecraft Flight to Phobos with a Perturbation Maneuver near the Moon, Based on the Solution of a Combination of 4 Lambert’s Problems / Proceedings of the 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS-2023). Saint Petersburg: IEEE, 2023. С. https://ieeexplore.ieee.org/document/10168493.