55427

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Статья в журнале/сборнике

Название: 

Minimum Fuel-Consumption Stabilization of a Spacecraft at the Lagrangian Points

ISBN/ISSN: 

0005-1179

Наименование источника: 

  • Automation and Remote Control

Обозначение и номер тома: 

Vol. 80, Iss. 12

Город: 

  • Berlin

Издательство: 

  • Pleades Publishing, Ltd.

Год издания: 

2019

Страницы: 

2217–2228
Аннотация
We consider the motion of a spacecraft described by the differential equations of the three-body problem in the Earth-Moon system. The goal is to stabilize the spacecraft in the neighborhood of the collinear Lagrangian points (which are know to be unstable equilibria) via use of minimum fuel-consumption control. The adopted approach is based on l1-optimization of linearized and discretized equations with terminal conditions being the target Lagrangian point. Therefore, the problem reduces to a linear program, and its solution defines pulse controls for the original three-body equations. Upon reaching the desired neighborhood, the spacecraft performs control-free flight until its deviation from the Lagrangian point exceeds certain prespecified threshold. The correction is then applied repeatedly, so that the spacecraft is kept within a small neighborhood of the unstable equilibrium point.

Библиографическая ссылка: 

Поляк Б.Т., Шалби Л.А. Minimum Fuel-Consumption Stabilization of a Spacecraft at the Lagrangian Points // Automation and Remote Control. 2019. Vol. 80, Iss. 12. С. 2217–2228.

Публикация имеет версию на другом языке или вышла в другом издании, например, в электронной (или онлайн) версии журнала: 

Да

Связь с публикацией: