Observer-based decoupling control of air flow and pressure in fuel cell systems

被引:0
作者
Yuan, Yupeng [1 ,2 ,3 ]
Xiong, Zhe [1 ,2 ,4 ]
Xue, Guoqing [1 ,2 ,4 ]
Tong, Liang [1 ,2 ,3 ]
Shen, Boyang [5 ]
机构
[1] Wuhan Univ Technol, State Key Lab Maritime Technol & Safety, Wuhan, Peoples R China
[2] Wuhan Univ Technol, Natl Engn Res Ctr Water Transport Safety, Wuhan, Peoples R China
[3] Wuhan Univ Technol, Reliabil Engn Inst, Sch Transportat & Logist Engn, Wuhan 430063, Hubei, Peoples R China
[4] Wuhan Univ Technol, Sch Naval Architecture Ocean & Energy Power Engn, Wuhan, Peoples R China
[5] Univ Cambridge, Dept Engn, Cambridge, England
基金
中国国家自然科学基金;
关键词
Marine fuel cell air supply system; Decoupling control; Diagonal decoupling matrix; Integral sliding mode control; EXCESS RATIO CONTROL; MANAGEMENT; DESIGN;
D O I
10.1016/j.ijhydene.2024.09.318
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
This paper investigates the control of the air supply system for marine proton exchange membrane fuel cells. A mathematical model of the air supply system is established, and a sliding mode diagonal decoupling controller based on a state observer is proposed. The control effectiveness is validated through experiments and simulations. A decoupling control strategy for the air supply system of marine fuel cells is presented. First, the load input current of the fuel cell system is selected according to the load characteristics of the target vessel, ensuring that the load current meets the power level of the fuel cell system model. Second, the impact of the cathode pressure on the fuel cell system is analyzed. An observer-based measurement method is proposed to address the measurement issue of cathode pressure. On this basis, a decoupling control strategy combining a diagonal decoupling matrix and sliding mode variable structure control theory is proposed. Finally, the effectiveness of the decoupling controller is validated through Matlab/Simulink. The results show the proposed decoupling controller exhibits superior performance to existing controllers with environmental disturbances, continuous time-varying loads, and step loads. The maximum relative error is 2.95%, the average relative error is 0.022%, and the longest adjustment time is 0.5 s. These results indicate that the control performance of the proposed decoupling controller is superior to that of diagonal PI controllers and sliding mode controllers, thereby validating the superiority of the sliding mode decoupling controller. This article provides a useful method for the development and application of control technology for the air supply system of marine fuel cells.
引用
收藏
页码:1075 / 1104
页数:30
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