gyroscopyГироскопия и навигацияGiroskopiya i Navigatsiya0869-70352075-0927AO «Концерн «ЦНИИ «Электроприбор»KEQWBGgyroscopy-119Research ArticleСтатьиАдаптивная система управления угловым движением малоразмерного космического аппаратаAn Adaptive Attitude Control System for Small SatellitesКрамлихА. В.KramlikhA. V.

Крамлих Андрей Васильевич. Кандидат технических наук, доцент. Член секции молодых ученых международной общественной организации «Академия навигации и управления движением»

Самарский национальный исследовательский университет имени академика С.П. КоролеваРоссияSamara National Research UniversityRussian Federation202520052025331106124Copyright © Крамлих А.В., 20252025Крамлих А.В.Kramlikh A.V.Данная работа распространяется под лицензией Creative Commons Attribution 4.0.This work is licensed under a Creative Commons Attribution 4.0 License.https://www.gyroscopy.ru/jour/article/view/119

В статье описывается подход к построению системы управления угловым движением малоразмерного космического аппарата (МКА), адаптивной к возможным отказам измерительных и исполнительных устройств. Метод основан на идее включения в контур системы ее цифрового двойника, предназначенного для детектирования отказов измерительных средств с использованием прогнозных значений измерений, которые рассчитываются по адаптивным бортовым моделям движения МКА. Такой подход увеличивает нагрузку на бортовые вычислительные средства МКА, однако позволяет предотвратить обработку недостоверных измерительных данных в контуре обратной связи. Компенсация отказа измерительных средств производится путем реконфигурации алгоритмического обеспечения, с помощью которого определяется ориентация МКА. Для компенсации отказов отдельных каналов исполнительных устройств предложен алгоритм управления угловым движением МКА, чья структура имеет вид четных рядов Фурье.

The paper describes an approach to designing an attitude control system for small spacecraft (SS), adaptive to possible failures of sensors and actuators. With this aim in view, the system loop includes its digital twin, which is designed to detect failures of measuring equipment using predicted measurement values calculated based on onboard adaptive SS motion models. This approach increases the SS onboard computational burden, but prevents processing of unreliable measurement data in the feedback loop. Compensation for the failure of sensors and actuators is performed by reconfiguring the algorithmic support used to determine the SS attitude. To compensate for failures of actuators’ individual channels, an algorithm for SS attitude control is proposed, the structure of which has the form of even Fourier series. 

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The authors declare that there are no conflicts of interest present.