Electrodynamic stabilization of artificial earth satellites in the König coordinate system
- Авторы: Aleksandrov A.1, Antipov K.1, Platonov A.1, Tikhonov A.1
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Учреждения:
- St. Petersburg State University
- Выпуск: Том 55, № 2 (2016)
- Страницы: 296-309
- Раздел: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219603
- DOI: https://doi.org/10.1134/S1064230716010020
- ID: 219603
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Аннотация
An artificial Earth satellite in a circular equatorial orbit is considered. We analyze the possibility of a satellite’s three-axis stabilization in the König coordinate system using an electrodynamic control system exploiting Lorentz and magnetic control torques. Conditions allowing the electromagnetic control to solve the problem for a gravitational torque disturbance are obtained. In the nonlinear formulation, sufficient conditions for the asymptotic stability of the satellite equilibrium position are obtained.
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Об авторах
A. Aleksandrov
St. Petersburg State University
Автор, ответственный за переписку.
Email: aleksandrov@spbu.ru
Россия, Universitetskaya nab. 7-9, St. Petersburg, 199034
K. Antipov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Россия, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Platonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Россия, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Tikhonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Россия, Universitetskaya nab. 7-9, St. Petersburg, 199034