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Tuesday 28 July 2020

A Comparative Study of Energy Management Schemes for a Fuel-Cell Hybrid Emergency Power System of More-Electric Aircraft


ABSTRACT:  
This paper presents a comparative analysis of different energy management schemes for a fuel-cell-based emergency power system of a more-electric aircraft. The fuel-cell hybrid system considered in this paper consists of fuel cells, lithium-ion batteries, and supercapacitors, along with associated dc/dc and dc/ac converters. The energy management schemes addressed are state of the art and are most commonly used energy management techniques in fuel-cell vehicle applications, and they include the following: the state machine control strategy, the rule-based fuzzy logic strategy, the classical proportional–integral control strategy, the frequency decoupling/fuzzy logic control strategy, and the equivalent consumption minimization strategy. The main criteria for performance comparison are the hydrogen consumption, the state of charges of the batteries/supercapacitors, and the overall system efficiency. Moreover, the stresses on each energy source, which impact their life cycle, are measured using a new approach based on the wavelet transform of their instantaneous power. A simulation model and an experimental test bench are developed to validate all analysis and performances.

KEYWORDS:
1.      Batteries
2.      Dc–dc converters
3.      Energy management
4.      Fuel cells
5.      Hybridization
6.      Optimization
7.      Supercapacitors
SOFTWARE: MATLAB/SIMULINK

BLOCK DIAGRAM:



Fig. 1 Proposed system block diagram using AFLC

 EXPERIMENTAL RESULTS:





Fig. 2. DC/DC converter model validation. (a) Fuel-cell boost converter. (b) Battery boost converter. (c) Battery buck converter.


Fig. 3 DC/AC converter model validation.


Fig. 4. Simulation and experimental results for all EMS schemes. (a) Simulation results for state machine control. (b) Experimental results for state machine
control. (c) Simulation results for rule-based fuzzy logic. (d) Experimental results for rule-based fuzzy logic. (e) Simulation results for classical PI control.
(f) Experimental results for classical PI control. (g) Simulation results for frequency decoupling and fuzzy logic. (h) Experimental results for frequency decoupling
and fuzzy logic. (i) Simulation results for ECMS. (j) Experimental results for ECMS.

CONCLUSION:
This paper has presented a performance comparison of different energy management schemes for a fuel-cell hybrid emergency system of MEA. The hybrid system is modeled and  validated with experiments. Five state-of-the-art commonly used energy management schemes are studied through simulations and experimental tests on a 14-kW fuel-cell hybrid  system. The same initial condition is used for all the schemes, and the experimental results are close to simulations. The criteria for performance comparison are the hydrogen consumption, the battery SOC, the overall efficiency, and the stress seen by each energy source. The latter is measured using a new approach based on wavelet transform. Compared with the other schemes, the state machine control scheme provided slightly better efficiency (80.72%) and stresses on the battery  and supercapacitor (σ of 21.91 and 34.7, respectively). The classical PI control scheme had the lowest fuel consumption (235 g of H2 consumed) and more use of the battery energy (SOC between 70%–51%). As expected, the lowest fuel-cell stress (σ of 12.04) and the lowest use of the battery energy (SOC between 70%–59%) were achieved with the frequency decoupling and fuzzy logic scheme but at the expense of more fuel consumption (245 g of H2 consumed) and lower overall efficiency (79.32%). The dc-bus or supercapacitor voltage was maintained nearly constant (270 Vdc) for all the schemes. To conclude, the energy management system suitable for MEA should be a multischeme EMS, such that each scheme is chosen based on a specific criterion to prioritize. As an example, depending on the operating life of each energy source, the EMS can be chosen to either minimize the stress on the fuelcell system, the battery system, or the supercapacitor system, hence maximizing the life cycle of the hybrid power system. In addition, if the target is to reduce the fuel consumption, the strategy based on the classical PI or ECMS could be selected. An alternative is to design a multiobjective optimization EMS  to optimize all the performance criteria, which is the next topic for further studies.

REFERENCES:
[1] P. Thounthong and S. Rael, “The benefits of hybridization,” IEEE Ind. Electron. Mag., vol. 3, no. 3, pp. 25–37, Sep. 2009.
[2] P. Thounthong, S. Rael, and B. Davat, “Control strategy of fuel cell and supercapacitors association for a distributed generation system,” IEEE  Trans. Ind. Electron., vol. 54, no. 6, pp. 3225–3233, Dec. 2007.
[3] Z. Amjadi and S. Williamson, “Power-electronics-based solutions for plug-in hybrid electric vehicle energy storage and management systems,” IEEE Trans. Ind. Electron., vol. 57, no. 2, pp. 608–616, Feb. 2010.
[4] G. Renouard-Vallet, M. Saballus, G. Schmithals, J. Schirmer, J. Kallo, and A. K. Friedrich, “Improving the environmental impact of civil aircraft  by fuel cell technology: Concepts and technological progress,” Energy  Environ. Sci., vol. 3, no. 10, pp. 1458–1468, 2010.
[5] G. Renouard-Vallet, M. Saballus, G. Schmithals, J. Schirmer, J. Kallo, and A. K. Friedrich, “Fuel cells for aircraft applications,” ECS Trans., vol. 30, no. 1, pp. 271–280, 2011.