gyroscopyГироскопия и навигацияGiroskopiya i Navigatsiya0869-70352075-0927AO «Концерн «ЦНИИ «Электроприбор»10.17285/0869-7035.0076gyroscopy-198Research ArticleСтатьиПредотвращение возможности возникновения резонансных режимов движения для низковысотных спутников класса CubeSatPreventing Resonant Motion Modes for Low-Altitude CubeSat Nanosatelliteshttps://orcid.org/0000-0002-4645-7212БариноваЕ. В.BarinovaE. V.

Баринова Елена Витальевна. Кандидат технических наук, доцент межвузовской кафедры космических исследований.

https://orcid.org/0000-0002-5486-8820БелоконовИ. В.BelokonovI. V.

Белоконов Игорь Витальевич. Доктор технических наук, профессор, заведующий межвузовской кафедрой космических исследований, действительный член общественного объединения «Академия навигации и управления движением». 

https://orcid.org/0000-0002-5074-1590ТимбайИ. А.TimbaiI. A.

Тимбай Иван Александрович. Доктор технических наук, профессор межвузовской кафедры космических исследований, действительный член общественного объединения «Академия навигации и управления движением».

Самарский национальный исследовательский университет имени академика С.П. КоролёваРоссияSamara National Research University, RussiaRussian Federation202122102025294115133Copyright © Баринова Е.В., Белоконов И.В., Тимбай И.А., 20252025Баринова Е.В., Белоконов И.В., Тимбай И.А.Barinova E.V., Belokonov I.V., Timbai I.A.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/198

Резонансные режимы движения, проявляющиеся в существенном увеличении амплитуды колебаний по пространственному углу атаки, могут привести к невыполнению целевой задачи полета. В связи с этим в статье исследуются резонансные режимы движения аэродинамически стабилизированных наноспутников формата CubeSat при полете на низких круговых орбитах при малой инерционно-массовой асимметрии. В отличие от осесимметричных тел вращения у наноспутников формата CubeSat резонансы могут проявляться не только из-за наличия малой асимметрии, но и по причине форм-фактора прямоугольного параллелепипеда. В работе получены формулы для определения критических значений продольной угловой скорости наноспутника, при которых выполняются условия возникновения резонансных режимов движения, а также предложен подход к предотвращению возможного появления резонансов для наноспутников класса CubeSat.

Resonant modes of motion, manifested as a significant increase in the oscillation amplitude of the spatial angle of attack, can result in the failure of the CubeSat mission. This paper is concerned with the study of the resonant motion modes of aerodynamically stabilized CubeSat nanosatellites in low circular orbits with small inertia and mass asymmetry. In contrast to axisymmetric bodies of rotation, resonances in CubeSat nanosatellites can be caused not only by small asymmetry, but they also arise due to the form factor of the rectangular parallelepiped. Formulas have been obtained to determine the critical values of the nanosatellite longitudinal angular velocity at which the conditions for the emergence of resonant motion modes are fulfilled. An approach is proposed to prevent possible resonances for CubeSat nanosatellites.

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