太阳能/氢能无人机总体设计与能源管理策略研究

doi:10.7527/S1000-6893.2015.0273

方案设计与多学科分析

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

太阳能/氢能无人机总体设计与能源管理策略研究

刘莉, 杜孟尧, 张晓辉, 张超, 徐广通, 王正平

北京理工大学宇航学院, 北京 100081

收稿日期:2015-08-20 修回日期:2015-10-12 出版日期:2016-01-25 发布日期:2015-10-26
通讯作者: 刘莉,Tel.:010-68914534,E-mail:liuli@bit.edu.cn E-mail:liuli@bit.edu.cn
作者简介:刘莉女,博士,教授。主要研究方向:飞行器总体设计、飞行器结构分析与设计、飞行动力学与控制。Tel:010-68914534,E-mail:liuli@bit.edu.cn;杜孟尧男,硕士研究生。主要研究方向:飞行器总体设计。Tel:010-68913290,E-mail:2120130043@bit.edu.cn;张晓辉男,博士研究生。主要研究方向:飞行器总体设计。Tel:010-68913290,E-mail:3120130031@bit.edu.cn

Conceptual design and energy management strategy for UAV with hybrid solar and hydrogen energy

LIU Li, DU Mengyao, ZHANG Xiaohui, ZHANG Chao, XU Guangtong, WANG Zhengping

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received:2015-08-20 Revised:2015-10-12 Online:2016-01-25 Published:2015-10-26

摘要/Abstract

摘要：

针对小型低空长航时电动无人机需求,给出了太阳能/氢能混合能源动力系统集成方案和小型低空长航时无人机构型。针对典型任务剖面,综合考虑太阳能电池和氢燃料电池特性,提出了一种考虑全机重量能量耦合关系的总体设计方法和任务剖面驱动的能源管理策略;建立了能源系统模型,给出了能源控制流程,开发了能源管理仿真平台。以1.5 kg任务载荷为例,完成了无人机总体方案设计,仿真分析了各种能源特性对飞行结果的影响。结果表明:能源管理策略能够根据任务剖面的要求合理配置能源系统的功率,满足各阶段的功率需求;无人机在冬至日航时为21 h、夏至日可实现跨昼夜飞行;在能源系统重量相同情况下,该混合能源无人机的航时分别是纯锂电池无人机和燃料电池无人机的5.5倍和1.2倍。

关键词: 太阳能, 氢能, 长航时, 电动无人机, 总体设计, 能源管理

Abstract:

According to the long-endurance demand of small low-altitude electric UAVs,a hybrid solar and hydrogen energy system and a configuration of long-endurance small low-altitude UAV is introduced.Based on the typical flight profile and the characteristics of solar cells and fuel cells,a conceptual design method which considers the coupling relationship of weight and energy and the corresponding profile-driven energy management strategy is proposed.Energy system models are built.Furthermore,an energy control procedure is provided,and a simulation platform for hybrid energy management is developed.For an instance,a configuration scheme of the UAV with 1.5 kg payload is achieved.Based on this case,the influences of the characteristics of the energy sources on the flight results are analyzed in the process of simulation.Results prove that the strategy of energy management is able to achieve an efficient power distribution in accordance with the flight profile as well as satisfies the power requirements of all stages.The endurance of the UAV reaches 21 h on winter solstice and a whole day and whole night on summer solstice.Under the same weight of energy systems,the endurance of the proposed hybrid-powered UAV is 5.5 times of the lithium battery powered UAV and 1.2 times of solar powered UAV,respectively.

Key words: solar energy, hydrogen energy, long endurance, electric powered UAV, conceptual design, energy management

中图分类号:

V221.2

刘莉, 杜孟尧, 张晓辉, 张超, 徐广通, 王正平. 太阳能/氢能无人机总体设计与能源管理策略研究[J]. 航空学报, 2016, 37(1): 144-162.

LIU Li, DU Mengyao, ZHANG Xiaohui, ZHANG Chao, XU Guangtong, WANG Zhengping. Conceptual design and energy management strategy for UAV with hybrid solar and hydrogen energy[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(1): 144-162.

参考文献

[1] 马东立,包文卓,乔宇航.利于冬季飞行的太阳能飞机构型研究[J].航空学报,2014,35(6):1581-1591.MA D L,BAO W Z,QIAO Y H.Study of solar-powered aircraft configuration beneficial to winter flight[J].Acta Aeronautica et Astronautica Sinica,2014,35(6):1581-1591(in Chinese).
[2] ZHU X,GUO Z,HOU Z.Solar-powered airplanes:A historical perspective and future challenges[J].Progress in Aerospace Sciences,2014,71:36-53.
[3] 邓海强,余雄庆.太阳能飞机的现状和发展趋势[J].航空科学技术,2006(1):28-30.DENG H Q,YU X Q.Solar aircraft:status and directions[J].Aeronautical Science and Technology,2006(1):28-30(in Chinese).
[4] 昌敏,周洲,郑志成.太阳能飞机原理及总体参数敏度分析[J].西北工业大学学报,2010,28(5):792-796.CHANG M,ZHOU Z,ZHENG Z C.Flight principles of solar-powered airplane and sensitivity analysis of its conceptual parameters[J].Journal of Northwestern Ploytechnical University,2010,28(5):792-796(in Chinese).
[5] NOTH A.Design of solar powered airplanes for continuous flight[D].Zürich:ETH Zürich,2008:1-17.
[6] SWIDER-LYONS K E,MACKRELL J A,RODGERS J A,et al.Hydrogen fuel cell propulsion for long endurance small UAVs[C]//Proceeding of the AIAA Centennial of Naval Aviation Forum "100 Years of Achievement and Progress".Reston:AIAA,2011:1-8.
[7] LTD H E S P.Aerostak data sheet[M].2015:1-3.
[8] VERSTRAETE D,GONG A,LU D D C,et al.Experimental investigation of the role of the battery in the AeroStack hybrid,fuel-cell-based propulsion system for small unmanned aircraft systems[J].International Journal of Hydrogen Energy,2015,40(3):1598-1606.
[9] VERSTRAETE D,LEHMKUEHLER K,GONG A,et al.Characterisation of a hybrid,fuel-cell-based propulsion system for small unmanned aircraft[J].Journal of Power Sources,2014,250:204-211.
[10] NOLL T B J,PEREZ DAVIS M.Investigation of the Helios Prototype Aircraft Mishap[R].Washington,D.C.:NASA,2004.
[11] HAO C,KHALIGH A.Hybrid energy storage system for unmanned aerial vehicle(UAV)[C]//Proceeding of the IECON 2010-36th Annual Conference on IEEE Industrial Electronics Society.Piscataway,NJ:IEEE Press,2010:2851-2856.
[12] BOHWA L,POOMIN P,KEUNBAE K.Power managements of a hybrid electric propulsion system for UAVs[J].Journal of Mechanical Science and Technology,2012,26(8):2291.
[13] BOHWA L,POOMIN P,KEUNBAE K,et al.The flight test and power simulations of an UAV powered by solar cells,a fuel cell and batteries[J].Journal of Mechanical Science and Technology,2014,28(1):399-405.
[14] BOHWA L,SEJIN K,POOMIN P,et al.Active power management system for an unmanned aerial vehicle powered by solar cells,a fuel cell,and batteries[J].IEEE Transactions on Aerospace and Electronic Systems,2014,50(4):3167-3177.
[15] LTD P H T C.EOS series data sheet[M].2011:2-7.
[16] LTD P H T C.PhyX series data sheet[M].2011:1-4.
[17] HERWERTH C,OFOMA U,WU D C,et al.Development of a fuel cell powered UAV for environmental research[C]//44th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA,2006:1-13.
[18] OFOMA U C,WU C C.Design of a fuel cell powered UAV for environmental research:AIAA-2004-6384[R].Reston:AIAA,2004.
[19] BIRD R E,HULSTRON R L.A simplified clear sky model for direct and diffuse insolation on horizontal surfaces[R].1981.
[20] 李延平.太阳能/氢能混合动力小型无人机总体设计[D].北京:北京理工大学,2014:65-71.LI Y P.Conceptual design for solar/hydrogen hybrid powered small-scale UAV[D].Beijing:Beijing Insititute of Technology,2014:65-71(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

太阳能/氢能无人机总体设计与能源管理策略研究

Conceptual design and energy management strategy for UAV with hybrid solar and hydrogen energy

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	王海峰, 刘坤澎, 江泓鑫, 杜晨曦. 螺旋桨多设计点气动优化方法和变桨距角策略[J]. 航空学报, 2024, 45(9): 528831-528831.
[2]	李广佳, 王红波, 张凯, 仪志胜. 临近空间太阳能无人机增升减阻技术综述[J]. 航空学报, 2024, 45(5): 529644-529644.
[3]	姬志行, 王占学, 程莉雯, 秦江, 刘禾. 燃料电池燃气涡轮航空混合推进系统总体性能及匹配分析[J]. 航空学报, 2024, 45(10): 129326-129326.
[4]	高显忠, 邓小龙, 王玉杰, 郭正, 侯中喜. 临近空间太阳能飞机能量最优飞行航迹规划方法展望[J]. 航空学报, 2023, 44(8): 27265-027265.
[5]	丁玉临, 韩忠华, 乔建领, 聂晗, 宋文萍, 宋笔锋. 超声速民机总体气动布局设计关键技术研究进展[J]. 航空学报, 2023, 44(2): 626310-626310.
[6]	史智广, 杨玉洁, 左宗玉. 多囊体临近空间飞艇多要素耦合建模与仿真[J]. 航空学报, 2023, 44(16): 228451-228451.
[7]	邵嘉琪, 张晓辉, 席涵宇, 刘子荣. 太阳能无人机线性自抗扰多环路能源控制[J]. 航空学报, 2023, 44(10): 327812-327812.
[8]	朱炳杰, 杨希祥, 宗建安, 邓小龙. 分布式混合电推进飞行器技术[J]. 航空学报, 2022, 43(7): 25556-025556.
[9]	赵欢, 高正红, 夏露. 高速自然层流翼型高效气动稳健优化设计方法[J]. 航空学报, 2022, 43(1): 124894-124894.
[10]	高明, 余伟臣, 王杉杉, 王荣闯, 石健将. 太阳能无人机能源系统的多维耦合建模[J]. 航空学报, 2021, 42(7): 224461-224461.
[11]	杜楠楠, 陈建, 马奔, 王术波, 张自超. 多太阳能无人机覆盖路径优化方法[J]. 航空学报, 2021, 42(6): 324476-324476.
[12]	范周伟, 余雄庆, 王朝, 钟伯文. 基于深度神经网络的客机总体设计参数敏感性分析[J]. 航空学报, 2021, 42(4): 524353-524353.
[13]	段登燕, 裴家涛, 祖瑞, 李建波. 电机-变距螺旋桨动力系统功率优化控制[J]. 航空学报, 2021, 42(3): 623933-623933.
[14]	张茂权, 陈海昕. 小型电动无人机航程航时估算模型[J]. 航空学报, 2021, 42(3): 625085-625085.
[15]	刘刚, 王正平, 刘莉, 张晓辉, 曹潇. 考虑局部遮挡的太阳能无人机能源控制[J]. 航空学报, 2020, 41(3): 623178-623178.