Design and sizing of electrical power source for a nanosatellite using photovoltaic cells
Design and sizing of electrical power source for a nanosatellite using photovoltaic cells
复制标题
使用光伏电池的纳米卫星电源的设计和尺寸确定
DOI：
10.1109/irsec.2015.7455059
复制
发表时间：
2015
期刊：
影响因子：
--
通讯作者：
M. Elhafyani
中科院分区：
文献类型：
--
作者：
S. Dahbi;A. Aziz;S. Zouggar;N. Benazzi;Hassan Zahboune;M. Elhafyani
尊重标准形状立方体卫星的纳米卫星由于其小的尺寸和表面积，目前面临着各种工程挑战。挑战是将大量的技术整合成不超过10cm3的立方体形式，并且只消耗1W。本文基于一种新的按情景计算的策略、电池提出的二次电源规范和功率控制分配单元(PCDU)，给出了光伏太阳能电池等电源(EPS)各部件的设计和尺寸。文中还给出了纳米卫星电力系统管理的仿真结果。
The nanosatelitte that respects the standard form CubeSat present various engineering challenges due to its small size and surface area. The challenge is to incorporate a large amount of technology in a cubic form no bigger than 10cm3 and consumes only 1W. In this paper, we present the design and sizing of all components of electrical power source (EPS) such as photovoltaic solar cells specifications based on a new strategy of calculation by scenario, secondary power sources specifications presented by the batteries, and power control distribution unit (PCDU). Also the simulation results for the management of the power system in the nanosatellite are displayed.