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Интеллектуальная Система Тематического Исследования НАукометрических данных |
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Stabilization of Satellite Relative Equilibrium Using MagneticMoments and Aerodynamic Forcesстатья
- Авторы: Morozov V.M., Kalenova V.I.
- Журнал: Cosmic Research (English translation of Kosimicheskie Issledovaniya)
- Том: 60
- Номер: 3
- Год издания: 2021
- Издательство: Pleiades Publishing, Inc.
- Местоположение издательства: New York, USA
- Первая страница: 213
- Последняя страница: 219
- DOI: 10.1134/S0010952522030066
- Аннотация: We consider the stabilization of the relative equilibrium of a satellite moving in a circular orbit, which is equipped with a magnetic attitude-control system, taking into account aerodynamic moments. It is shown that the linearized system of equations of motion belongs to a special class of linear time-varuing systemsthat are reducible to time-invariant ones. The controllability of the system of both time-invariant and time-varuingsystems is investigated. The efficient optimal stabilization algorithm based on the reduced time-invariant systemis constructed. A detailed simulation is carried out that demonstrates the effect of aerodynamic moments.
- Добавил в систему: Каленова Вера Ильинична