17608

Автор(ы): 

Автор(ов): 

3

Параметры публикации

Тип публикации: 

Доклад

Название: 

Linear feedback spacecraft stabilization using the method of invariant ellipsoids

ISBN/ISSN: 

0094-2898

Наименование конференции: 

  • 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA)

Наименование источника: 

  • Proceedings of the 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA)

Город: 

  • Туллахома, США

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2009

Страницы: 

195-198, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=4806834
Аннотация
This paper addresses the robust attitude control for an uncertain flexible spacecraft with disturbances bounded by ellipsoids. An observed-state feedback is designed using the so-called invariant ellipsoid method, which is based on the local invariant set theorem. The minimum invariant ellipsoid can be considered as the influence of the uncertainties and disturbances in the controlled system. All these considerations were expressed through LMI technique as an optimization problem with linear objective and LMI constraints. The numerical solution of this problem gives the parameters for the linear controller and the Luenberger observer that guarantee a quasi-minimal invariant ellipsoid for the controlled spacecraft.

Библиографическая ссылка: 

Гонсалес-Гарсия С., Поляков А.Е., Позняк А.С. Linear feedback spacecraft stabilization using the method of invariant ellipsoids / Proceedings of the 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA). Туллахома, США: Institute of Electrical and Electronics Engineers (IEEE), 2009. С. 195-198, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=4806834.