Stabilization of spacecraft orbital attitude
Автор: Zubov Nickolay Eugenevich, Lapin Alexey Vladimirovich, Mikrin Evgeny Anatolyevich
Журнал: Космическая техника и технологии @ktt-energia
Рубрика: Бортовые и наземные комплексы управления и системы
Статья в выпуске: 3 (3), 2013 года.
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The paper discusses the problem of spacecraft orbital stabilization when the body-fixed reference system is misaligned with respect to the principal axes of inertia. Using the exact pole placement technique, analytical expressions were obtained for the feedback controller matrix of the spacecraft orbital stabilization problem.
Orbital stabilization, inertia tensor, exact pole placement method
Короткий адрес: https://sciup.org/14343424
IDR: 14343424
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