Electrodynamic stabilization of artificial earth satellites in the König coordinate system
- Авторлар: Aleksandrov A.1, Antipov K.1, Platonov A.1, Tikhonov A.1
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Мекемелер:
- St. Petersburg State University
- Шығарылым: Том 55, № 2 (2016)
- Беттер: 296-309
- Бөлім: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219603
- DOI: https://doi.org/10.1134/S1064230716010020
- ID: 219603
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
A. Aleksandrov
St. Petersburg State University
Хат алмасуға жауапты Автор.
Email: aleksandrov@spbu.ru
Ресей, Universitetskaya nab. 7-9, St. Petersburg, 199034
K. Antipov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Ресей, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Platonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Ресей, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Tikhonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
Ресей, Universitetskaya nab. 7-9, St. Petersburg, 199034