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论文:2012,Vol:30,Issue(6):868-873 |
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引用本文: |
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肖伟, 周洲, 王睿, 李满. 分布式推进系统对太阳能无人机横航向飞行品质的影响研究[J]. 西北工业大学 |
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Xiao Wei, Zhou Zhou, Wang Rui, Li Man. Effectively Determining Some Selected Effects of Distributed Propulsion System on Lateral Flight Quality of Solar UAV[J]. Northwestern polytechnical university |
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分布式推进系统对太阳能无人机横航向飞行品质的影响研究 |
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肖伟1, 周洲1, 王睿1, 李满2 |
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1. 西北工业大学 无人机特种技术重点实验室, 陕西 西安 710072; 2. 空军航空大学 航空理论系, 吉林 长春 130022 |
摘要: |
文章根据太阳能无人机推进系统的特点,建立了电机螺旋桨的数学模型。通过分析系统产生的推力随飞行状态的变化关系,以及推进系统在大展弦比飞翼式太阳能无人机上的分布,采用线性化方法,计算了分布式的推进系统对高空长航时太阳能无人机飞行品质的影响。研究了分布式推进系统分布位置、控制方式等与无人机飞行品质之间的关系。从飞行品质要求和推进系统的整体效率出发,对各推进系统的参数进行了选取,最后通过非线性模型对分析结果进行了仿真验证。 |
关键词:
太阳能无人机
飞行品质
电机
螺旋桨
参数优化
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Effectively Determining Some Selected Effects of Distributed Propulsion System on Lateral Flight Quality of Solar UAV |
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Xiao Wei1, Zhou Zhou1, Wang Rui1, Li Man2 |
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1. National Key Laboratory of Science and Technology on UAV, Northwestern Polytechnical University Xi'an 710072; 2. China Aviation University of Airforce, Changchun 130022, China |
Abstract: |
Sections 1 through 3 of the full paper explain the determination of the effects mentioned in the title and then propose an optimization scheme based on such determined effects; we believe that both our determination andoptimization scheme mentioned above are effective. The core of Sections 1 through 3 consists of: (1) we establishthe mathematical model for the motor-propeller propulsion system of HALE solar UAV; (2) we analyze the relation-ship between flight conditions and output thrust of the distributed propulsion system; (3) we linearize the model,and, based on the study of flight quality of large aspect-ratio solar UAV, deduce the effects of distributed propulsionsystem on lateral flight quality of the solar UAV,which are altered by the distribution and control scheme of propul-sion system; (4) for the purpose of long flight endurance,we propose an optimization scheme; (5) simulation re-sults,presented in Figs. 5 through 7,and their analysis show preliminarily that our optimization scheme is indeedeffective. |
Key words:
aspect ratio
computer simulation
damping
DC motors
efficiency
eigenvalues and eigenfunctions
flight dynamics
linearization
mathematical models
optimization
propellers
propulsion
schematicdiagrams
solar energy
stability
unmanned aerial vehicles(UAV);flight quality
parameter optimi-zation
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收稿日期: 2011-12-10
修回日期:
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DOI: |
基金项目: 国家自然科学基金(11202162)资助 |
通讯作者:
Email: |
作者简介: 肖伟(1982-),西北工业大学博士研究生,主要从事飞行动力学与控制的研究。
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相关功能 |
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作者相关文章 |
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肖伟 在本刊中的所有文章 |
周洲 在本刊中的所有文章 |
王睿 在本刊中的所有文章 |
李满 在本刊中的所有文章 |
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参考文献: |
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[1] Kirk Flittie,Bob Curtin.Pathfinder Solar-Powered Aircraft Flight Performance.AIAA-1998-4446 [2] Mark Drela.Integrated Simulation Model for Preliminary Aerodynamic,Structural and Control-Law Design of Aircraft.AIAA-1999-1394 [3] 刘沛清.空气螺旋桨理论及其应用.北京:北京航空航天大学出版社, 2006, 45-54Liu Peiqing.Theory and Application of Aero Propeller.Beijing: Beijing University of Aeronautics and Astronautics Press,2006, 45-54 (in Chinese) [4] 胡文华, 彭 韬, 陆云波等.无位置传感器无刷直流电动机的调速控制方式.微电机, 2004, 37(2): 28-32Hu Wenhua,Peng Tao,Lu Yunbo,et al.Analyse of Position-Sensorless BLDCM Speed Control Mode.Micro Motor, 2004, 37(2): 28-32 (in Chinese) [5] 方振平等.航空飞行器飞行动力学.北京: 北京航空航天大学出版社, 2005Fang Zhenping,et al.Aircraft Flight Dynamics.Beijing: Beijing University of Aeronautics and Astronautics Press,2005 (inChinese) [6] 赵 凯.总体设计中太阳能飞机的建模与仿真: [硕士学位论文].西安: 西北工业大学, 2011Zhao Kai.Modeling and Simulation of Solar-Powered Airplane for the Major Phase of Design.Master Degree Dissertation.Xi'an: Northwestern Polytechnical University, 2011 (in Chinese) |
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