[1]段海滨,范彦铭,张雷.高空长航时无人机技术发展新思路[J].智能系统学报,2012,7(03):195-199.
 DUAN Haibin,FANG Yanming,ZHANG Lei.New thoughts on the development of a HALE UAV[J].CAAI Transactions on Intelligent Systems,2012,7(03):195-199.
点击复制

高空长航时无人机技术发展新思路(/HTML)
分享到:

《智能系统学报》[ISSN:1673-4785/CN:23-1538/TP]

卷:
第7卷
期数:
2012年03期
页码:
195-199
栏目:
出版日期:
2012-06-25

文章信息/Info

Title:
New thoughts on the development of a HALE UAV
文章编号:
1673-4785(2012)03-0195-05
作者:
段海滨12范彦铭3张雷4
1.北京航空航天大学 自动化科学与电气工程学院,北京 100191;
2.北京航空航天大学 飞行器控制一体化技术重点实验室,北京 100191;
3.中国航空工业集团公司 沈阳飞机设计研究所,辽宁 沈阳 110035;
4.中国人民解放军 空军装备部,北京 100843
Author(s):
DUAN Haibin12 FANG Yanming3 ZHANG Lei4
1.School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;
2. Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China;
3. Shenyang Aircraft Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110035, China;
4. Air Force Arming Department, People’s Liberation Army, Beijing 100843, China
关键词:
高空长航时无人机 多目标组合优化 气动〖KG-*1/3〗-〖KG-*1/5〗隐身一体化 软件使能自主控制 多机分布协同
Keywords:
HALE UAV multiobjective optimization integrated design of aerodynamic and stealthy performance softwareenabled control multiplatform distributed cooperation
分类号:
TP273
文献标志码:
A
摘要:
根据未来航空发展的战略需要,面向新一代高空长航时无人机的系统设计,十分有必要开展探索性、创新性和面向高空长航时无人机的关键技术研究.提出了高空长航时无人机技术发展的新思路和其瓶颈问题的解决方案.重点从高空长航时无人机多目标组合优化、气动〖KG-*1/3〗-〖KG-*1/3〗隐身一体化、能源动力、软件使能自主控制、自主导航、测控和信息传输、空天地多机分布协同等方面给出了可行技术方案和重点研究方向.这些技术的实现可增强高空长航时无人机系统方面的可持续发展能力,支撑和引领相关领域的技术发展.
Abstract:
According to the strategic requirements of future aviation development, and considering system design for the new generation of highaltitude and longendurance (HALE) unmanned aerial vehicles (UAVs), it is necessary to develop exploratory, innovative, and key technologies for HALE UAVs. In this paper, some new ideas were proposed for HALE UAVs which mainly focus on multiobjective optimization, integrated design of aerodynamic and stealthy performance, energy and power, softwareenabled control, autonomous navigation, measurement and control systems, information transmission, and multiplatform distributed cooperation. The proposed technologies can enhance the capacity of HALE UAV systems for sustainable development, and support the developments in other relevant technical areas. 

参考文献/References:

[1]TUZCU I, MARZOCCA P, CESTINO E, et al. Stability and control of a highaltitude, longendurance UAV[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 713721.
[2]ATREYA S, MATA M, JONES R, et al. Power system comparisons for a high altitude long endurance (HALE) remotely operated aircraft (ROA)[C]//AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO). Arlington, USA, 2005: AIAA20057401.
[3]AGTE J, COHEN K. First order effects of new technology on a high altitude long endurance (HALE) unmanned aerial vehicle (UAV)[C]//Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno, USA, 2008: AIAA2008168.
[4]PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelasticity and flight dynamics of highaltitude longendurance aircraft[J]. Journal of Aircraft, 2001, 38(1): 8894.
[5]CARNIE G, QIN N. Fluidstructure interaction of HALE wing configuration with an efficient moving grid method[C]//Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno, USA, 2008: AIAA2008309.
[6]TUZCU I, MARZOCCA P, AWNI K. Nonlinear dynamical modeling of a high altitude long endurance unmanned aerial vehicle[C]//Proceedings of the 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials. Palm Springs, USA, 2009: AIAA20092404.
[7]GRAY D. Design and integration of antennas with prototype HALE UAVs[C]//Proceedings of the 25th AIAA International Communications Satellite Systems. Seoul, Korea, 2007: AIAA20073143.
[8]NICKOL C L, GUYNN M D, KOHOUT L L, et al. High altitude long endurance air vehicle analysis of alternatives and technology requirements development[C]//Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit. Reno, USA, 2007: AIAA20071050.
[9]SIVAJI R, GHIA U, GHIA K N, et al. Aerodynamic analysis of the joinedwing configuration of a HALE aircraft[C]//Proceedings of the 41st Aerospace Sciences Meeting and Exhibit. Reno, USA, 2003: AIAA2003606.
[10]李珂.长航时无人机机翼平面参数及翼型选择分析[J].飞行力学, 2007, 25(3): 911, 16.
 LI Ke. A study on wing geometry and airfoils effects for long eudurance unmanned aircraft[J]. Flight Dynamics, 2007, 25(3): 911, 16.
[11]曹秋生,张会军.高空长航时无人机的发展特点及技术难点探讨[J].中国电子科学研究院学报, 2008, 3(1): 813.
CAO Qiusheng, ZHANG Huijun. Characteristics of HALE UAVs in development and discussion of existing technical difficulties[J]. Journal of China Academy of Electronics and Information Technology, 2008, 3(1): 813.
[12]郭科志.鸭式布局高空长航时无人机系列的概念设计与气动优化[D].南京:南京航空航天大学, 2008: 3435.
GUO Kezhi. Conceptual design and aerodynamic optimization for UAV family with canard configuration[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008: 3435.
[13]邱玉鑫,程娅红,胥家常.浅析高空长航时无人机的气动研究问题[J].流体力学实验与测量, 2004, 18(3): 15.
QIU Yuxin, CHENG Yahong, XU Jiachang. A brief discussion of highaltitude longendurance unmanned aerial vehicle aerodynamic research[J]. Experiments and Measurements in Fluid Mechanics, 2004, 18(3): 15.
[14]赵刚,蔡元虎,屠秋野,等.高空长航时无人机用涡扇发动机技术分析[J].推进技术, 2009, 30(2): 154158, 181.
ZHAO Gang, CAI Yuanhu, TU Qiuye, et al. Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicle[J]. Journal of Propulsion Technology, 2009, 30(2): 154158, 181.
[15]DUAN Haibin, SHAO Shan, SU Bingwei, et al. New development thoughts on the bioinspired intelligence based control for unmanned combat aerial vehicle[J]. Science China: Technological Sciences, 2010, 53(8): 20252031.
[16]吴海仙,俞文伯,房建成.高空长航时无人机SINS/CNS组合导航系统仿真研究[J].航空学报, 2006, 27(12): 299304.
WU Haixian, YU Wenbo, FANG Jiancheng. Simulation of SINS/CNS integrated navigation system used on high altitude and longflighttime unpiloted aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(12): 299304.
[17]周姜滨,袁建平,罗建军,等.高空长航时无人机导航系统研究[J].西北工业大学学报, 2008, 26(4): 463467.
ZHOU Jiangbin, YUAN Jianping, LUO Jianjun, et al. Navigation system of HALE UAV (high altitude long endurance unmanned aerial vehicle) suitable for China[J]. Journal of Northwestern Polytechnical University, 2008, 26(4): 463467.
[18]林伟廷.高空长航时无人机侦察任务规划问题研究[D].长沙:国防科学技术大学, 2007: 8789.
 LIN Weiting. Research on high altitude and long endurance unmanned aerial vehicle reconnaissance mission planning[D]. Changsha: National University of Defense Technology, 2007: 8789.

备注/Memo

备注/Memo:
收稿日期: 2011-11-29.
基金项目:国家自然科学基金资助项目(60975072);教育部新世纪优秀人才支持计划资助项目(NCET10021);航空科学基金资助项目(20115151019);北京科技新星计划资助项目(2007A017) .
通信作者:段海滨. E-mail: hbduan@buaa.edu.cn.
作者简介:
段海滨,男,1976年生,副教授,博士生导师,博士,主要研究方向为无人机自主控制与智能决策、计算机仿生视觉等.主持国家自然科学基金3项、国家“863”计划4项、航空科学基金3项,作为第一完成人获省部级科技进步一等奖、二等奖、三等奖各1项,曾入选教育部新世纪优秀人才计划、北京市科技新星计划.发表学术论文40余篇,其中被SCI检索30余篇.
范彦铭,男,1964年生,研究员,中航工业沈阳飞机设计研究所副总设计师,中航工业集团首席专家,主要研究方向为先进飞行控制系统.先后荣获国防科学技术进步特等奖、一等奖各1次、二等奖4次,荣立部级一等功1次、二等功2次、三等功1次,曾被授予“沈阳市青年科技先锋”称号,发表学术论文20余篇. 
张雷,男,1978年生,中国人民解放军空军装备部参谋,博士,主要研究方向为无人机任务规划与自主控制、发动机控制等.获省部级科技进步二等奖2次,发表学术论文20余篇.
更新日期/Last Update: 2012-09-05