纳米卫星低成本多电子负载样机的研制与测试

Limam Lakhdar, Boutte Aissa, Bentoutou Houari, Belaidi El Yazid
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引用次数: 1

摘要

纳米卫星以其体积小、重量轻、速度快、团队小、开发成本低的特点,正在成为卫星的新时代。然而,即使有这些优势,在日食期间仍然需要使用电池作为辅助电源。这些电池需要经过良好的选择,才能在特定环境下进行测试,并集成到纳米卫星中。在选择过程中,甚至在测试过程中,电池需要多次放电和充电,这需要一个电子负载,这是非常昂贵的。本文基于商用电子负载的相同技术,提出了一种低成本的电子负载原型。所提出的电子负载是为航空航天应用开发的锂离子电池试验台的一部分,它有三种不同的模式:恒流、恒功率和恒电阻。最终的原型将被复制,以便有几个电子负载,这将允许同时测试多个电池单元,减少所需的时间和精力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development and Testing of Low-Cost Multi-Electronic Load Prototype for Nanosatellites
Nanosatellites are becoming the new age of satellites for their small size, lightweight, fast and low-cost development within a small team. However, even with those advantages, it is still needed to use batteries as a secondary power source during eclipses. Those batteries require a good selection before being tested under a specific environment and integrated within the Nanosatellite. During the selection procedure or even during testing, batterie’s cells need to be discharged and charged several times requiring an electronic load, this one very expensive. In this paper, a low-cost electronic load prototype has been proposed based on the same technology for commercial electronic loads. The proposed electronic load is part of a Lithium-Ion battery test bench developed for aerospace applications, it has three different modes: Constant Current, Constant Power, and Constant Resistor. The final prototype will be duplicated in order to have several electronic loads, which will allow for the simultaneous testing of multiple battery cells, reducing the time and effort required.
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