52786

Автор(ы): 

Автор(ов): 

4

Параметры публикации

Тип публикации: 

Статья в журнале/сборнике

Название: 

Terminal synthesis of orbital orientation for a spacecraft

Электронная публикация: 

Да

ISBN/ISSN: 

1555-6530

DOI: 

10.1134/S1064230717040190

Наименование источника: 

  • Journal of Computer and Systems Sciences International

Обозначение и номер тома: 

Vol. 56, Iss. 4

Город: 

  • Род-Таун

Издательство: 

  • Springer Link

Год издания: 

2017

Страницы: 

721–737
Аннотация
This paper presents an algorithm for the terminal synthesis of the orbital orientation for a spacecraft. The algorithm is based on solving the following problems: the analytical determination of the program values for the angular velocity vector components in an orbital coordinate system and the stabilization of the program values for the turn rate vector components and the desired terminal angular position of a spacecraft. The program values of the angular velocity vector components are determined analytically using the method previously proposed by the authors for solving a boundary value problem based on the parameter identification of a discrete model with the use of modal control. The simulation results demonstrating the effectiveness of the proposed algorithm, as well as the high accuracy level of the steady-state control, are presented.

Библиографическая ссылка: 

Зубов Н.Е., Ли М.В., Микрин Е.А., Рябченко В.Н. Terminal synthesis of orbital orientation for a spacecraft / Journal of Computer and Systems Sciences International. Род-Таун: Springer Link, 2017. Vol. 56, Iss. 4. С. 721–737.

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