Modeling the Angular Motion Dynamics of Small Spacecraft with a Magnetic Attitude Control System in a Three-Axis Stabilization Mode

被引：0
|
作者：
Kulkov, V. M. [1 ]
Egorov, Yu G. [1 ]
Firsyuk, S. O. [1 ]
Terentyev, V. V. [1 ]
Shemyakov, A. O. [1 ]
机构：
[1] Natl Res Univ, Moscow Aviat Inst, Moscow 119334, Russia
来源：
DOKLADY PHYSICS | 2019年 / 64卷 / 10期
关键词：
655.1; Spacecraft; General - 701.2 Magnetism: Basic Concepts and Phenomena - 731.1 Control Systems - 731.3 Specific Variables Control;
D O I：
10.1134/S1028335819100021
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The problem of modeling the attitude control modes of small spacecraft using electromagnetic systems interacting with the Earth's magnetic field is considered. A mathematical model for the angular motion dynamics of small spacecraft has been developed. The control law for linear magnetic attitude control systems of small spacecraft is formulated. The results of our numerical modeling of the motion of a satellite with a magnetic attitude control system are presented.
引用
收藏
页码：389 / 393
页数：5
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