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Full Length Article | Open Access

Distributed power conditioning unit of large-scale space solar power station

Xintong LIa,b,Jianwei MIa,b( )Yiqun ZHANGa,bGuanheng FANb,cJie DUa,b
School of Mechano-electronic Engineering, Xidian University, Xi’an 710071, China
Shaanxi Key Laboratory of Space Solar Power Station System, Xidian University, Xi’an 710071, China
Academy of Advanced Interdisciplinary Research, Xidian University, Xi’an 710071, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

In this paper, a multi-bus distributed Power Conditioning Unit (PCU) is proposed for the Space Solar Power Station with large scale photovoltaic (PV) array and power levels reaching MW level. In this unit, there are multiple independent PV arrays. In each PV array, there are multiple independent PV subarrays. In this paper, a V-P droop control method with adaptive droop coefficient is proposed, which modifies the droop intercept based on the bus voltage deviation and the power per unit value of the PV array. This method ensures the accuracy of bus voltage and achieves proportional distribution of power between PV arrays based on the proposed topology structure in this paper. When the load changes or the output power of the PV array fluctuates, this method can ensure that power is distributed proportionally. The principle and control method of the proposed droop control method is analyzed in this paper. The effectiveness of the method is verified through MATLAB/Simulink simulation and experiment. Simulation and experimental results show that the proposed method can achieve power distributed proportionally when load changes and PV output power fluctuates, reduce bus voltage error caused by line impedance and differences in rated power of different PV arrays, and improve the performance of PV power generation system applied to space.

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Chinese Journal of Aeronautics
Pages 421-434
Cite this article:
LI X, MI J, ZHANG Y, et al. Distributed power conditioning unit of large-scale space solar power station. Chinese Journal of Aeronautics, 2024, 37(8): 421-434. https://doi.org/10.1016/j.cja.2024.05.020

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Received: 20 September 2023
Revised: 16 October 2023
Accepted: 06 February 2024
Published: 23 May 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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