Electrodynamic stabilization of artificial earth satellites in the König coordinate system
- 作者: Aleksandrov A.1, Antipov K.1, Platonov A.1, Tikhonov A.1
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隶属关系:
- St. Petersburg State University
- 期: 卷 55, 编号 2 (2016)
- 页面: 296-309
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219603
- DOI: https://doi.org/10.1134/S1064230716010020
- ID: 219603
如何引用文章
详细
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.
作者简介
A. Aleksandrov
St. Petersburg State University
编辑信件的主要联系方式.
Email: aleksandrov@spbu.ru
俄罗斯联邦, Universitetskaya nab. 7-9, St. Petersburg, 199034
K. Antipov
St. Petersburg State University
Email: aleksandrov@spbu.ru
俄罗斯联邦, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Platonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
俄罗斯联邦, Universitetskaya nab. 7-9, St. Petersburg, 199034
A. Tikhonov
St. Petersburg State University
Email: aleksandrov@spbu.ru
俄罗斯联邦, Universitetskaya nab. 7-9, St. Petersburg, 199034