Maximizing solar energy input for Cubesat using sun tracking system and a maximum power point tracking

Hammam Abdelwahab, M. Nawari, Hanadi Abdalla
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引用次数: 8

Abstract

For any Cubesat the Power System Unit is designed to deliver the required energy so as the nano-satellite can achieve its desired mission. Thus the input energy for the solar panels and the output energy from the solar cells must be increased. The sun tracking system aims to maximize the input solar energy to the solar panels. This paper aims to study the concept of designing sun tracking solar panels and a maximum power point tracker for the UOKSAT-3 Cubesat which is a 2 units Cubesat with a deployable solar panels. The paper details the effectiveness and importance of the tracking process, the impacts of the tracking mechanism on the Attitude Determination and Control and their interfacings to rotate the Cubesat. This paper also presents the MPPT's performance and its results to study the change of the input energy using the (MPPT).
利用太阳跟踪系统和最大功率点跟踪,使立方体卫星的太阳能输入最大化
对于任何立方体卫星,动力系统单元的设计都是为了提供所需的能量,以便纳米卫星能够完成其预期的任务。因此,太阳能电池板的输入能量和太阳能电池的输出能量必须增加。太阳跟踪系统的目的是最大限度地提高太阳能电池板的输入能量。本文旨在研究UOKSAT-3立方体卫星的太阳跟踪太阳能电池板和最大功率点跟踪器的设计概念。UOKSAT-3立方体卫星是一个带有可展开太阳能电池板的2单元立方体卫星。本文详细介绍了跟踪过程的有效性和重要性,跟踪机制对姿态确定和控制的影响以及它们对立方体卫星旋转的接口。本文还介绍了MPPT的性能及其结果,以研究使用MPPT时输入能量的变化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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