期刊
IEEE TRANSACTIONS ON POWER ELECTRONICS
卷 37, 期 1, 页码 629-643出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TPEL.2021.3098584
关键词
CubeSat; Topology; Radiation effects; Inductors; Switches; DC-DC power converters; Maximum power point trackers; CubeSats; electric power system (EPS) design; low earth orbit (LEO) satellites; nanosatellites; small satellites; switched capacitor converter (SCC)
资金
- Khalifa University, AbuDhabi, UAE [02/MI/MIT/CP/11/07633/GEN/G/00]
- Advanced Power Energy Center (APEC) at Khalifa University
- Massachusetts Institute of Technology (MIT), Cambridge, MA, USA [02/MI/MIT/CP/11/07633/GEN/G/00]
A single-inductor-based multiport converter topology is proposed for the electric power system of LEO CubeSats. This topology allows for maximum solar power extraction from each PV panel under varying irradiation conditions.
Maximization of solar energy harvest and miniaturization of dc-dc converters are essential for low earth orbit (LEO) CubeSats, which are constrained by volume and weight restrictions. The state-of-the-art electric power system (EPS) architectures utilize several individual dc-dc converters to maximize solar energy harvest but it has a tradeoff with miniaturization as it requires several inductors. The main objective of this article is to propose a single-inductor-based multiport converter topology for the LEO CubeSat's EPS. The proposed topology interfaces the photovoltaic (PV) panels to the energy storage system and a control strategy have been developed to extract maximum solar power from each PV panel under wide varying irradiation conditions of the LEO CubeSat. The proposed topology consists of series-connected half-bridge modules fed by PV panels and their output is supplied to the energy storage system via a boost converter. The principle of operation is introduced followed by steady-state analysis and converter dynamics analysis. The performance of the proposed converter is verified for several case studies with an experimental prototype developed based on 1U CubeSat specifications.
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