Abstract

The angular motion of a CubeSat-type nanosatellite with a passive magnetic attitude control system is mathematically modelled. The attitude control system consists of a permanent magnet and hysteresis dampers in the form of a plate or a set of rods. The parameters of the hysteresis dampers are studied using a laboratory facility. A comparative analysis of the damping time using the plate and the set of rods is presented.

中文翻译：

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使用迟滞板对纳米卫星的角运动阻尼建模

摘要

数学上模拟了具有无源磁姿态控制系统的CubeSat型纳米卫星的角运动。姿态控制系统由一块永磁体和一组板或一组杆形式的磁滞阻尼器组成。使用实验室设备研究磁滞阻尼器的参数。给出了使用板和一组杆的阻尼时间的比较分析。