Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite
HAPS (high-altitude pseudosatellites) are flight machines, airplane type, generally without pilot which fly in a definite zone at 18-22 km altitude, providing communication and surveillance services. These flight machines do not leave the atmosphere, and their purpose is to maintain a constant fligh...
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Series: | Modelling and Simulation in Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/5459098 |
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doaj-c74144b551094159b50d830093a275402020-11-25T03:18:55ZengHindawi LimitedModelling and Simulation in Engineering1687-55911687-56052020-01-01202010.1155/2020/54590985459098Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude PseudosatelliteJ. I. Corcau0L. Dinca1Department of Electrical, Energetic and Aerospace Engineering, University of Craiova, Craiova 200440, RomaniaDepartment of Electrical, Energetic and Aerospace Engineering, University of Craiova, Craiova 200440, RomaniaHAPS (high-altitude pseudosatellites) are flight machines, airplane type, generally without pilot which fly in a definite zone at 18-22 km altitude, providing communication and surveillance services. These flight machines do not leave the atmosphere, and their purpose is to maintain a constant flight level for as long time as possible in the interest zone (e.g., five years) to fulfill their mission. HAPS energetic system proposed in this paper has to feed the electric propulsion system of HAPS (12.5 kW) and also to feed on-board equipment (navigation, data links, scientific equipment, etc.). On-board energy sources have to maintain HAPS in the interest zone for long periods. For this reason, it is used in the present solar power sources. A part of the generated energy is consumed on board; the rest is stored daytime and consumed nighttime. So, the system is provided with energy generation systems and also with storage and management systems. HAPS energetic system is a hybrid type, with two or more power sources. In this case, power sources are photovoltaic panels are used daytime and fuel cell are used nighttime, and also, a battery and/or a supercapacitor is used in transition periods from day to night and in peak load periods. In this paper, an electric power system used nighttime is designed and analysed. In this situation, the primary power source is the fuel cell and the secondary power sources are battery and/or supercapacitor. There are used numerical simulations models, developed in Matlab/Simulink, for all hybrid power source components: fuel cell stack, battery system, supercapacitors, conversion system, and fuzzy logic power management system. For a part of these components, there are used existing simulation models in Matlab/Simulink, adapted to these simulation requirements, and for others, there are designed and implemented simulation schemes according to these simulation requirements. An important component of the hybrid power source is the power conversion system which adapts the power sources parameters to consumer input requirements. A fuzzy logic power management system is designed.http://dx.doi.org/10.1155/2020/5459098 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
J. I. Corcau L. Dinca |
spellingShingle |
J. I. Corcau L. Dinca Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite Modelling and Simulation in Engineering |
author_facet |
J. I. Corcau L. Dinca |
author_sort |
J. I. Corcau |
title |
Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite |
title_short |
Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite |
title_full |
Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite |
title_fullStr |
Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite |
title_full_unstemmed |
Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite |
title_sort |
fuzzy energy management scheme for a hybrid power sources of high-altitude pseudosatellite |
publisher |
Hindawi Limited |
series |
Modelling and Simulation in Engineering |
issn |
1687-5591 1687-5605 |
publishDate |
2020-01-01 |
description |
HAPS (high-altitude pseudosatellites) are flight machines, airplane type, generally without pilot which fly in a definite zone at 18-22 km altitude, providing communication and surveillance services. These flight machines do not leave the atmosphere, and their purpose is to maintain a constant flight level for as long time as possible in the interest zone (e.g., five years) to fulfill their mission. HAPS energetic system proposed in this paper has to feed the electric propulsion system of HAPS (12.5 kW) and also to feed on-board equipment (navigation, data links, scientific equipment, etc.). On-board energy sources have to maintain HAPS in the interest zone for long periods. For this reason, it is used in the present solar power sources. A part of the generated energy is consumed on board; the rest is stored daytime and consumed nighttime. So, the system is provided with energy generation systems and also with storage and management systems. HAPS energetic system is a hybrid type, with two or more power sources. In this case, power sources are photovoltaic panels are used daytime and fuel cell are used nighttime, and also, a battery and/or a supercapacitor is used in transition periods from day to night and in peak load periods. In this paper, an electric power system used nighttime is designed and analysed. In this situation, the primary power source is the fuel cell and the secondary power sources are battery and/or supercapacitor. There are used numerical simulations models, developed in Matlab/Simulink, for all hybrid power source components: fuel cell stack, battery system, supercapacitors, conversion system, and fuzzy logic power management system. For a part of these components, there are used existing simulation models in Matlab/Simulink, adapted to these simulation requirements, and for others, there are designed and implemented simulation schemes according to these simulation requirements. An important component of the hybrid power source is the power conversion system which adapts the power sources parameters to consumer input requirements. A fuzzy logic power management system is designed. |
url |
http://dx.doi.org/10.1155/2020/5459098 |
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AT jicorcau fuzzyenergymanagementschemeforahybridpowersourcesofhighaltitudepseudosatellite AT ldinca fuzzyenergymanagementschemeforahybridpowersourcesofhighaltitudepseudosatellite |
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