gyroscopyГироскопия и навигацияGiroskopiya i Navigatsiya0869-70352075-0927AO «Концерн «ЦНИИ «Электроприбор»10.17285/0869-7035.2018.26.3.069-091gyroscopy-286Research ArticleСтатьиАнализ и синтез движения аэродинамически стабилизированных космических аппаратов нанокласса формата CUBESATAnalysis and Synthesis of Motion of Aerodynamically Stabilized Nanosatellites of the CubeSat DesignБелоконовИ. В.BelokonovI. V.

Белоконов Игорь Витальевич. Доктор технических наук, профессор, заведующий межвузовской кафедрой космических исследований.

Действительный член общественного объединения «Академия навигации и управления движением».

ТимбайИ. А.TimbaiI. A.

Тимбай Иван Александрович. Доктор технических наук, профессор, профессор межвузовской кафедры космических исследований.

Действительный член общественного объединения «Академия навигации и управления движением».

НиколаевП. Н.NikolaevP. N.

Николаев Петр Николаевич. Аспирант межвузовской кафедры космических исследований

Самарский национальный исследовательский университет имени академика С. П. КоролёваРоссияInter-University Department of Space Research Samara National Research University, Samara, RussiaRussian Federation2018211120252636991Copyright © Белоконов И.В., Тимбай И.А., Николаев П.Н., 20252025Белоконов И.В., Тимбай И.А., Николаев П.Н.Belokonov I.V., Timbai I.A., Nikolaev P.N.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/286

Исследуется движение аэродинамически стабилизированных космических аппаратов нанокласса формата CubeSat. Отмечаются особенности поведения наноспутников на низких орбитах, обусловленные как влиянием атмосферы, так и присущими им массово-инерционными характеристиками. Срок существования наноспутников меньше, а угловое ускорение, порождаемое аэродинамическим моментом, значительно больше, чем у спутников с существенными размерами и массой. У наноспутников формата CubeSat возможно возникновение резонансных режимов движения, обусловленных присущим им форм-фактором прямоугольного параллелепипеда. Кроме того, существующие коммерческие пусковые устройства отделения наноспутников, как правило, порождают большие величины начальной угловой скорости, которые носят случайный характер.

В работе выявлены и проанализированы условия, порождающие особенности в движении такого класса космических аппаратов, предложен вероятностный подход к выбору их массовых и инерционных характеристик, исследованы проблемы стабилизации движения и сформированы рекомендации по формированию облика аэродинамически стабилизированного наноспутника формата CubeSat с пассивно-активной магнитной системой гашения колебаний.

The motion of aerodynamically stabilized nanosatellites of the CubeSat design is studied. The features of the nanosatellites behavior in low orbits are conditioned both by the atmospheric effects and their own mass and inertial characteristics: the lifetime of nanosatellites is shorter, while the angular acceleration generated by the aerodynamic moment is much higher as compared with big satellites having large mass. CubeSats may experience resonance modes of motion caused by the shape factor of a rectangular parallelepiped. In addition, the existing commercial CubeSat deployers often generate large initial angular velocities that are random in nature. The conditions that cause the specific features of the CubeSat motion are considered and analyzed. A probabilistic approach to choosing their mass and inertial characteristics is proposed. The problems of motion stabilization are studied, and recommendations are formulated on the design of aerodynamically stabilized CubeSats with a passive/active magnetic damping system.

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