电子电气工程与控制

燃料电池无人机混合电源动态平衡能量管理策略

  • 雷涛 ,
  • 闵志豪 ,
  • 付红杰 ,
  • 张星雨 ,
  • 李伟林 ,
  • 张晓斌
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  • 1. 西北工业大学 自动化学院, 西安 710129;
    2. 西北工业大学 航空学院, 西安 710129;
    3. 飞机电推进技术工信部重点实验室, 西安 710129

收稿日期: 2020-04-02

  修回日期: 2020-05-18

  网络出版日期: 2020-08-03

基金资助

国家自然科学基金(51877178)

Dynamic balanced energy management strategies for fuel-cell hybrid power system of unmanned air vehicle

  • LEI Tao ,
  • MIN Zhihao ,
  • FU Hongjie ,
  • ZHANG Xingyu ,
  • LI Weilin ,
  • ZHANG Xiaobin
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  • 1. School of Automation, Northwestern Polytechnical University, Xi'an 710129, China;
    2. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710129, China;
    3. Key laboratory of Aircraft Electric Propulsion Technology, Ministry of Industry and Information Technology, Xi'an 710129, China

Received date: 2020-04-02

  Revised date: 2020-05-18

  Online published: 2020-08-03

Supported by

National Natural Science Foundation of China (51877178)

摘要

飞机电推进的动力系统趋于混合能源形式的发展方向,不同类型的源具有不同的特性,混合能源协调工作的方式可以提高动力系统的性能。本文所研究的飞机电推进系统的能源形式为燃料电池和锂电池所做成的混合能源。针对无人机动力系统工况的特殊性,本文在基于规则的能量管理策略研究基础上,提出了一种基于燃料电池氢气消耗的动态平衡能量管理策略,使燃料电池和辅助电源的能量消耗处于相对平衡的状态,避免了其中一种电源能量先耗尽的情况,可以满足多种工况的变化,提高了混合电源的能量利用率和稳定性,保证了无人机动力系统的可靠性。通过仿真分析结果证明了可行性,最后设计了能量管理系统的硬件并进行了实验验证,通过对实验结果计算分析验证了该能量管理策略的可行性。

本文引用格式

雷涛 , 闵志豪 , 付红杰 , 张星雨 , 李伟林 , 张晓斌 . 燃料电池无人机混合电源动态平衡能量管理策略[J]. 航空学报, 2020 , 41(12) : 324048 -324048 . DOI: 10.7527/S1000-6893.2020.24048

Abstract

The propulsion system of aircraft electric propulsion tends to develop in the form of mixed energy. Different types of sources have different characteristics. The coordinated work of mixed energy can improve the performance of the power system. The energy form of the aircraft electric propulsion system studied in this paper is a hybrid energy source made of fuel cells and lithium batteries. In view of the particularity of the working conditions of the UAV power system, based on the above rule-based energy management strategy research, this paper proposes a dy-namic balance energy management strategy based on fuel cell hydrogen consumption to make the fuel cell and auxiliary power energy The consumption is in a relatively balanced state, which avoids the situation where one of the power sources is depleted first, can meet the changes of various working conditions, improves the energy utili-zation and stability of the mixed power source, and ensures the reliability of the UAV power system. The results of simulation analysis prove the feasibility. Finally, the hardware of the energy management system is designed and verified by experiments. The feasibility of the energy management strategy is verified by calculation and analysis of the experimental results.

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