Triaxial electrodynamic stabilization of a satellite via PID controller:

Александр Юрьевич Александров; Сергей Борисович Рузин

doi:10.21638/spbu10.2024.209

Авторы

Александр Юрьевич Александров Санкт-Петербургский государственный университет, Российская Федерация, 199034, Санкт-Петербург, Университетская наб., 7–9 https://orcid.org/0000-0001-7186-7996
Сергей Борисович Рузин Санкт-Петербургский государственный университет, Российская Федерация, 199034, Санкт-Петербург, Университетская наб., 7–9

DOI:

https://doi.org/10.21638/spbu10.2024.209

Аннотация

Рассматривается спутник, движущийся по круговой экваториальной орбите. Спутник оснащен управляемым магнитным моментом и управляемым электростатическим зарядом. Исследована задача трехосной стабилизации спутника в орбитальной системе координат. Предложена электродинамическая система управления. Кроме того, для улучшения характеристик переходных процессов используется ПИД-регулятор специальной формы. С помощью прямого метода Ляпунова получены условия асимптотической устойчивости программного режима. Приведены результаты компьютерного моделирования, демонстрирующие эффективность разработанного подхода.

Ключевые слова:

спутник, электродинамическое управление, трехосная стабилизация, функционал Ляпунова — Красовского, ПИД-регулятор

Скачивания

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Библиографические ссылки

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