Energy management strategy for solar-powered high-altitude long-endurance aircraft

被引:96
作者
Gao Xian-Zhong [1 ]
Hou Zhong-Xi [1 ]
Guo Zheng [1 ]
Liu Jian-Xia [1 ]
Chen Xiao-Qian [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China
关键词
Energy management strategy; High-altitude long-endurance aircraft; Control and structural system; Lithium-sulfur battery; Solar cell; ELECTROCHEMICAL PROPERTIES; CATHODE MATERIAL; MULTI-PAYLOAD; FUZZY-LOGIC; DESIGN; SYSTEM; PERFORMANCE; EFFICIENCY; COMPOSITE; ALGORITHM;
D O I
10.1016/j.enconman.2013.01.007
中图分类号
O414.1 [热力学];
学科分类号
摘要
Development of solar-powered High-Altitude Long-Endurance (HALE) aircraft has a great impact on both military and civil aviation industries since its features in high-altitude and energy source can be considered inexhaustible. Owing to the development constraints of rechargeable batteries, the solar-powered HALE aircraft must take amount of rechargeable batteries to fulfill the energy requirement in night, which greatly limits the operation altitude of aircraft. In order to solve this problem, a new Energy Management Strategy (EMS) is proposed based on the idea that the solar energy can be partly stored in gravitational potential in daytime. The flight path of HALE aircraft is divided into three stages. During the stage I, the solar energy is stored in both lithium-sulfur battery and gravitational potential. The gravitational potential is released in stage 2 by gravitational gliding and the required power in stage 3 is supplied by lithium-sulfur battery. Correspondingly, the EMS is designed for each stage. The simulation results show that the aircraft can always keep the altitude above 16 km with the proposed EMS, and the power consumed during night can be also alleviated. Comparing with the current EMS, about 23.5% energy is remained in batteries with the proposed EMS during one day-night cycle. The sensitivities of the improvement of crucial technologies to the performance of aircraft are also analyzed. The results show that the enhancement of control and structural system, lithium-sulfur battery, and solar cell are ranked in descending order for the performance improvement of solar-powered HALE aircraft. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:20 / 30
页数:11
相关论文
共 57 条
[51]  
Tuzcu I, 2006, 47 AIAA ASME ASCE AH, P1641
[52]   Charge/discharge characteristics of sulfurized polyacrylonitrile composite with different sulfur content in carbonate based electrolyte for lithium batteries [J].
Wang, Li ;
He, Xiangming ;
Li, Jianjun ;
Chen, Min ;
Gao, Jian ;
Jiang, Changyin .
ELECTROCHIMICA ACTA, 2012, 72 :114-119
[53]  
Winiecki J, 1999, AIRCRAFT DESIGN, V2, P19
[54]  
Xu LF, 2012, INT J HYDROGEN ENERG, DOI DOI 10.1016/J.IJHYDENE.2012.07.074>
[55]   Investigation of hydrogen usage in aviation industry [J].
Yilmaz, Ilker ;
Ilbas, Mustafa ;
Tastan, Murat ;
Tarhan, Cevahir .
ENERGY CONVERSION AND MANAGEMENT, 2012, 63 :63-69
[56]   Configurations analysis for high-altitude/long-endurance airships [J].
Yu, Daren ;
Lv, Xiaowu .
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2010, 82 (01) :48-59
[57]   Fuzzy logic based energy management strategy for commercial buildings integrating photovoltaic and storage systems [J].
Zhang, He ;
Davigny, Arnaud ;
Colas, Frederic ;
Poste, Yvan ;
Robyns, Benoit .
ENERGY AND BUILDINGS, 2012, 54 :196-206