41699

Автор(ы): 

Автор(ов): 

3

Параметры публикации

Тип публикации: 

Статья в журнале/сборнике

Название: 

Stabilization of low-frequency vibrations of a large satellite structure with powered gyro control

DOI: 

10.1134/S0005117913030077

Наименование источника: 

  • Automation and Remote Control

Обозначение и номер тома: 

Т. 74 вып. 3

Город: 

  • Москва

Издательство: 

  • SP MAIK Nauka/Interperiodica

Год издания: 

2013

Страницы: 

413-425
Аннотация
This paper considers the feasibility of using a discrete-time proportional-plus-derivative (PD) algorithm as a control law of gyrodyns for eliminating the drawback of their frames precession in the stabilization mode of the angular position of a deformable spacecraft. Moreover, we analyze dynamics features of applying such approach to control orientation of the above class of spacecrafts under "infralow" (0.01-0.1 Hz) frequencies of flexible vibrations of their structure. Finally, the issues concerning organization of a subsystem of additional gyro stabilization for weakly damped low-frequency vibrations are treated.

Библиографическая ссылка: 

Рутковский В.Ю., Суханов В.М., Глумов В.М. Stabilization of low-frequency vibrations of a large satellite structure with powered gyro control // Automation and Remote Control. 2013. Т. 74 вып. 3 . С. 413-425.

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