基于磁姿态控制系统的小型航天器三轴稳定姿态动力学建模

Доклады Академии наук Pub Date : 2019-10-10 DOI:10.31857/s0869-56524884377-382

V. M. Kulkov, В М Кульков, Yu. G. Egorov, Ю Г Егоров, S. O. Firsyuk, С. О. Фирсюк, V. V. Terentyev, В В Терентьев, A. Shemyakov, А О Шемяков

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摘要

考虑了利用与地球磁场相互作用的电磁系统对小型航天器姿态控制模式进行建模的问题。建立了小型航天器角运动数学模型。建立了小型航天器磁姿态控制系统的控制律。给出了卫星磁姿态控制系统运动数值模拟的结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Modelling the attitude dynamics of small spacecraft with a magnetic attitude control system in three-axis stabilization mode

The problem of modeling the attitude-control modes of small spacecraft with the use of electromagnetic systems, interacting with the Earths magnetic field is considered. A small spacecraft angular motion mathematical model is developed. A control law for magnetic attitude control system of small spacecraft is formulated. Results of satellite with magnetic attitude control system movement numerical modelling are presented.

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Доклады Академии наук

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