航天器太阳能电池阵在MPPT和DET方法下的功率评估指标

Zhang Xuan, Kang Qing, Y. Wentao, Xing Jie, Li Feng, You Xiangan
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引用次数: 2

摘要

为了定量测量最大功率点跟踪(MPPT)和三种不同直接能量转移(DET)方案下太阳能电池阵列的功率利用率,本文定义了能量损失百分比(ELP)和能量过剩百分比(EEP)两个功率指标,作为卫星电力系统设计的基础。根据光伏与蓄电池联运的特点、控制效率和设计余量,给出了这两个指标的计算方法。在ELP和EPP的基础上,分析了MPPT和DET体系结构的两种适用案例。计算结果表明,MPPT的ELP更好,而DET的EEP更具竞争力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Power Assessment Indices of Solar Arrays under MPPT and DET methods for Spacecraft
In order to measure power utilization ratio of solar arrays under Maximum Power Point Tracking(MPPT) and three different Direct Energy Transfer(DET) solutions quantitatively, this paper defines two power indices, energy loss percentage(ELP) and energy excess percentage(EEP), as the basis of satellite power system design. This paper also gives the calculation of these two indices based on the feature of joint-operation of PV and batteries, the control efficiency and the design margin. On the basis of ELP and EPP, two applicable cases of MPPT and DET architecture are analyzed. Computation results show that ELP of MPPT is better while EEP of DET is more competitive.
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