航空航天应用锂离子电池试验台研制

Boutte Aissa, Limam Lakhdar, Bourroua Benzina Med, Belaidi El Yazid, Mokhtar Ait Amirat, E. Bensikaddour
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引用次数: 1

摘要

在太空任务中,卫星根据轨道的每个阶段或季节提供所需的电力,直到其寿命结束。为了维持任务,我们应该确定电池组的尺寸,并进行资格和集成测试,以涵盖任务(低地球轨道- leo、地球同步转移轨道- gto、中地球轨道- meo或地球静止轨道- geo)的固定功率预算。卫星星载能量动力系统(EPS)的发展在选择将模块集成到航天飞行子系统之前需要进行验证和鉴定阶段。在这项工作中,我们提出了解决方案,以满足CubeSat电能存储模块的特定测试需求,这是通过开发测试系统模拟器来接近其轨道运行。所提出的系统由一个平台(硬件/软件)组成,允许预先选择用于太空任务的电池单元(锂离子,LiPo技术)通过预定义和可重构的循环或充放电微循环在轨道上与卫星相同的约束条件下生活,这些循环可以循环直到卫星寿命结束(EOL)。这项工作使我们能够在卫星任务的特定环境(受控温度)中进行电池测试,对锂离子电池进行耐久性和特性测试,以使其有资格用于空间系统。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Lithium-Ion Battery test bench development for Aerospace Applications
During a space mission, the satellite is supplied with required electrical power depending on each phase of the orbit or season, until its End-Of-Life. To maintain the mission, we should size well the battery-pack and proceed to the qualification and integration tests to cover the power budget fixed to the mission (Low Earth orbit-LEO, Geosynchronous Transfer orbit-GTO, Medium Earth orbit-MEO or Geostationary earth orbit-GEO). The development of the on-board energy power system (EPS) of satellite requires validation and qualification phases before opting for the modules to be integrated into aerospace flight subsystem. In this work we propose solution to cover the specific testing need of the electrical energy storage module of CubeSat, this by developing a test system emulator to get closer and closer to its orbit operating. The proposed system consists of a platform (Hardware / Software) allowing to the battery cells (Li-Ion, LiPo technologies) pre-selected for space mission to live the same constraints of the satellite in orbit through predefined and reconfigurable cycles or micro-cycles of charge/discharge, which can be looped until the end of satellite life (EOL). This work allows us to carry out batteries tests in a specific environment (controlled temperature) for a satellite mission, to perform endurance and characterization tests on Lith-Ion cells in order to qualify them for use in space systems.
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