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首页> 外文期刊>Doklady. Physics >Modeling the Angular Motion Dynamics of Spacecraft with a Magnetic Attitude Control System Based on Experimental Studies and Dynamic Similarity
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Modeling the Angular Motion Dynamics of Spacecraft with a Magnetic Attitude Control System Based on Experimental Studies and Dynamic Similarity

机译:基于实验研究和动态相似性的磁姿态控制系统建模航天器角度运动动力学

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摘要

The problem of spacecraft attitude control using electromagnetic systems interacting with the Earth's magnetic field is considered. A set of dimensionless parameters has been formed to investigate the spacecraft orientation regimes based on dynamically similar models. The results of experimental studies of small spacecraft with a magnetic attitude control system can be extrapolated to the in-orbit spacecraft motion control regimes by using the methods of the dimensional and similarity theory.
机译:考虑了使用与地球磁场相互作用的电磁系统的航天器姿态控制的问题。 已经形成了一组无量纲参数,以根据动态类似的模型来研究航天器取向制度。 通过使用尺寸和相似性理论的方法,可以将小型航天器与磁姿态控制系统的实验研究结果推断到轨道航天器运动控制方案。

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