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Синтез Нелинейного Закона Управления Для Перезакрутки Упругого Спутника Слабыми Внутренними Моментами

Author

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  • Сомов Евгений Иванович

    (НИИ проблем надежности механических систем, Самарский государственный технический университет)

Abstract

Рассмотрены принципиальные аспекты синтеза закона управления для перезакрутки спутника с целью совмещения вектора угловой скорости, направленного по оси наибольшего момента инерции его корпуса, с произвольно заданным направлением в инерциальной системе координат. Используются только слабые внутренние управляющие моменты, которые формируются силовым гироскопическим комплексом с ограниченными ресурсами.The paper considers principle aspects of control law synthesis for respinup of a satellite to combine the angular rate vector, directed on its body maximum inertia axis, with any given unit into inertial reference frame. Only weak internal torques are applied and the torques are generated by gyromoment cluster with bounded resources.

Suggested Citation

  • Сомов Евгений Иванович, 2013. "Синтез Нелинейного Закона Управления Для Перезакрутки Упругого Спутника Слабыми Внутренними Моментами," Проблемы управления, CyberLeninka;Общество с ограниченной ответственностью "СенСиДат-Контрол", issue 1, pages 63-69.
  • Handle: RePEc:scn:009530:14050957
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