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Design, implementation, and thermal modeling of embedded reconfigurable magnetorquer system for nanosatellites

机译:用于纳米卫星的嵌入式可重构磁矩系统的设计,实现和热建模

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摘要

A reconfigurable magnetorquer coil has been designed and implemented for the CubeSat power management, attitude determination, and control tile (CubePMT) module of CubeSat-standard nanosatellites. Magnetorquer coil is a good choice for attitude control and stabilization of nanosatellites. The goal of this work is to provide CubeSat with a magnetorquer coil, which has small dimensions, low weight, and low heat dissipation. The designed magnetorquer coil is reconfigurable and integrated within the printed circuit board internal layers, occupying no extra space on CubeSat. Coils in each layer are treated separately and can be attached and detached through straps. Changing the arrangement of these straps, one can use 1, 2, 3, or 4 coils in series, parallel, or any hybrid combination. This reconfigurable design provides an option for generating different amounts of magnetic moment and resultant torque to stabilize and rotate the satellite. Emissivity of the CubePMT module was found through lab experiments. Power dissipation and the corresponding temperature increase of the CubePMT module are evaluated by thermal modeling.
机译:已经为CubeSat标准纳米卫星的CubeSat电源管理,姿态确定和控制图块(CubePMT)模块设计并实现了可重构的磁矩线圈。磁矩线圈是控制姿态和稳定纳米卫星的理想选择。这项工作的目的是为CubeSat提供一个磁矩线圈,该线圈尺寸小,重量轻且散热低。设计的磁矩线圈是可重新配置的,并集成在印刷电路板的内部层中,在CubeSat上不占用任何额外空间。每层中的线圈都经过单独处理,可以通过皮带连接和分离。改变这些带子的布置,可以使用串联,并联或任何混合组合的1、2、3或4个线圈。这种可重新配置的设计提供了一个选项,用于生成不同数量的磁矩和合成转矩,以稳定和旋转卫星。通过实验室实验发现了CubePMT模块的发射率。通过热模型评估了CubePMT模块的功耗和相应的温度升高。

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