无人直升机飞行品质要求探讨

陈南宇; 蒙志君; 黄俊

doi:10.13700/j.bh.1001-5965.2015.0125

无人直升机飞行品质要求探讨

doi: 10.13700/j.bh.1001-5965.2015.0125

北京航空航天大学航空科学与工程学院, 北京 100083

基金项目: 北京高等学校青年英才计划项目(29201421)

详细信息

作者简介:
陈南宇男,博士研究生。主要研究方向:鲁棒控制理论及应用,飞行控制技术。 E-mail:nanyu_chan@126.com;蒙志君男,博士,副教授。主要研究方向:飞行器总体设计,飞行器雷达隐身技术,无人机总体/建模/控制/仿真技术。Tel.:010-82315584 E-mail:mengzhijun@buaa.edu.cn;黄俊男,博士,教授,博士生导师。主要研究方向:飞行器总体设计、隐身技术。

通讯作者:
蒙志君,Tel.:010-82315584 E-mail:mengzhijun@buaa.edu.cn

中图分类号: V279
计量
- 文章访问数: 907
- HTML全文浏览量: 35
- PDF下载量: 636
- 被引次数: 0
出版历程
- 收稿日期: 2015-03-09
- 网络出版日期: 2016-02-20

Research on flying quality of unmanned helicopter

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 针对无人直升机发展过程中对无人直升机飞行品质要求日益加剧,而相关领域的研究及成果甚少等问题,从自动飞行控制视角出发,较为系统地研究了无人直升机飞行品质涉及的各个基本方面,包括无人直升机飞行品质的定义、研究内容、影响因素和指标体系等;同时,通过对ADS-33E的合理改进,提出了适用于无人直升机飞行品质评估的三维架构以及相应的评估准则;可为新型无人直升机系统的研制和评估提供指导,为我国无人直升机飞行品质规范的早日出台提供借鉴。
- 无人直升机 /
- 飞行品质 /
- 飞行模态 /
- 评估准则 /
- 三维架构
Abstract: Considering the growing attention for flying qualities of unmanned helicopter while with little work and poor results in this field, the basic aspects of flying quality requirements of unmanned helicopter were discussed systematically, from the view of automatic flying control, such as the definition, research contents,influencing factors, indicators and so on; meanwhile, by rational improvements based on ADS-33E, a three-dimensional frame and the corresponding evaluation criteria suited to unmanned helicopter flight quality assessment were presented. It could provide guidance for the development and evaluation of a new unmanned helicopter system, or reference for the flying quality specification of unmanned helicopter being introduced early.
- unmanned helicopter /
- flying quality /
- flight mode /
- evaluation criteria /
- three-dimensional frame

HTML全文

参考文献(18)

[1]	BASKETT B J.Aeronautical design standard performance specification handling qualities requirements for military rotorcraft:ADS-33E-PRF[R].Alabama:United States Army Aviation and Missile Command Redstone Arsenalal,2000.
[2]	BLANKEN C L,HOH R H,MITCHELL D G,et al.Test guide for ADS-33E-PRF:AMR-AF-08-07[R].Arlington:U.S.Army RDECOM Special Report,2008.
[3]	中华人民共和国航空工业部.军用直升机飞行品质规范:HB 610586[S].北京:航空工业出版社,1986. Aerospace Industry Ministry.Military helicopter flying qualities specification:HB 610586[S].Beijing:Aviation Industry Press,1986(in Chinese).
[4]	DOWNS J,PRENTICE R,DALZELL S,et al.Control system development and flight test experience with the MQ-8B fire scout vertical take-off unmanned aerial vehicle(VTUAV)[C]//Proceedings of the American Helicopter Society(AHS) 63rd Annual Forum,2007.
[5]	Defence Standard 00-970 Design and Airworthiness Requirements for Service Aircraft Issue 4.Part 9:UAV Systems[Z].UK Ministry of Defence,2006.
[6]	高金源,焦宗夏,张平.飞机电传操纵系统与主动控制技术[M].北京:北京航空航天大学出版社,2005:74. GAO J Y,JIAO Z X,ZHANG P.Fly-by-wire control system and active control technology of aircraft[M].Beijing:Beihang University Press,2005:74(in Chinese).
[7]	文传源.现代飞行控制[M].北京:北京航空航天大学出版社,2004:59-61. WEN C Y.Modern flight control system[M].Beijing:Beihang University Press,2004:59-61(in Chinese).
[8]	昂海松,曾建江,童明波.现代航空工程[M].北京:国防工业出版社,2012:139. ANG H S,ZENG J J,TONG M B.Modern aeronautical engineering[M].Beijing:National Defense Industry Press,2012:139(in Chinese).
[9]	高正,陈仁良.直升机飞行动力学[M].北京:科学出版社,2003:143-146. GAO Z,CHEN R L.Helicopter flight dynamics[M].Beijing:Science Press,2003:143-146(in Chinese).
[10]	陈廷楠.飞机飞行性能品质与控制[M].北京:国防工业出版社,2007:66-67. CHEN T N.Aircraft flight performance quality and control[M].Beijing:National Defense Industry Press,2007:66-67(in Chinese).
[11]	程鹏.自动控制原理[M].2版.北京:高等教育出版社,2010:10-11. CHENG P.Automatic control theory[M].2nd ed.Beijing:Higher Education Press,2010:10-11(in Chinese).
[12]	曹义华.直升机飞行力学[M].北京:北京航空航天大学出版社,2005:92-96. CAO Y H.Helicopter flight mechanics[M].Beijing:Beihang University Press,2005:92-96(in Chinese).
[13]	陈仁良,高正.基于ADS-33的直升机纵向操纵响应研究[J].南京航空航天大学学报,2003,35(3):231-236. CHEN R L,GAO Z.Investigation of helicopter longitudinal control response based on ADS-33 requirements[J].Journal of Nanjing University of Aeronautics and Astronautics,2003,35(3):231-236(in Chinese).
[14]	军用直升机飞行品质规范背景材料和使用说明[M].北京:航空工业出版社,1986:5. Military helicopters flying qualities specification background material and instructions[M].Beijing:Aviation Industry Press,1986:5(in Chinese).
[15]	董庚寿.有人驾驶飞机(固定翼)飞行品质背景才料和使用说明[Z].国防科工委航空气动力协作公关办公室,1993. DONG G S.Manned aircraft(fixed wing) flying qualities background materials and instructions[Z].National Defense Aviation Aerodynamics Collaborative Public Relations Office,1993(in Chinese).
[16]	高金源,李陆豫,冯亚昌.飞机飞行品质[M].北京:国防工业出版社,2003:55. GAO J Y,LI L Y,FENG Y C.Aircraft quality[M].Beijing:National Defense Industry Press,2003:55(in Chinese).
[17]	单家元,孟秀云,丁艳.半实物仿真[M].北京:国防工业出版社,2008:18-72. SHAN J Y,MENG X Y,DING Y.HIL simulation[M].Beijing:National Defense Industry Press,2008:18-72(in Chinese).
[18]	刘林.现代飞行控制系统的评估与确认方法[M].北京:国防工业出版社,2010:69-75. LIU L.Advanced verification and clearance techniques for modern fligt control systems[M].Beijing:National Defense Industry Press,2010:69-75(in Chinese).