基于任务的飞机大迎角飞行品质评定准则

侯天俊; 郭有光; 王立新

doi:10.13700/j.bh.1001-5965.2014.0682

基于任务的飞机大迎角飞行品质评定准则

doi: 10.13700/j.bh.1001-5965.2014.0682

1.
北京航空航天大学中法工程师学院, 北京 100191
2. 北京航空航天大学航空科学与工程学院, 北京 100191

详细信息

作者简介:
侯天俊(1990—),男,河南开封人,硕士研究生,tianjun.hou@buaa.edu.cn

通讯作者:
王立新(1965—),男,江西南丰人,教授,wlx_c818@163.com,主要研究方向为飞机总体设计、新概念布局飞机动态特性与先进控制设计、民机飞行动力学与飞行安全.

中图分类号: V221.13
计量
- 文章访问数: 1113
- HTML全文浏览量: 83
- PDF下载量: 786
- 被引次数: 0
出版历程
- 收稿日期: 2014-11-04
- 网络出版日期: 2015-09-20

Mission-oriented flying qualities criteria for high angle of attack aircraft

1.
Sino-French Engineering School, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. School of Aeronautics Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 针对现代战斗机大迎角飞行品质缺少量化评定准则的问题,在常规飞行品质评定准则的基础上,采用基于任务的飞行品质评定方法,通过主观评估和客观评估,对多个具有不同电传操纵特性的飞机进行飞行品质评定,由此建立了定量的横向和纵向的大迎角飞行品质评定准则.将所得到的基于任务的大迎角飞行品质评定准则与常规飞行品质评定准则对比,结果表明:具有更大阻尼比和更大短周期操纵期望参数,在横向具有更大滚转模态时间常数的飞机,其大迎角飞行品质等级更优.建立的这一准则更适用于战斗机大迎角飞行的飞行品质评定研究,并可作为现代战斗机的设计标准.
- 大迎角 /
- 飞行品质 /
- 评定准则 /
- 基于任务 /
- 战斗机
Abstract: The flying qualities evaluation of high angle of modern attack aircraft lacks of quantitative evaluation criteria. Based on the conventional flying qualities criteria, with mission-oriented flying qualities evaluation method, various flying by wire systems with different transfer function parameters were tested, by subjective evaluation method and objective evaluation method. Thus, quantitative longitudinal and lateral flying qualities criteria for high angle of attack aircraft were developed. The result of comparison between the conventional flying qualities evaluation criteria and the quantitative evaluation criteria for high angle of attack aircraft shows that with higher short period damping ratio and control anticipate parameter in longitudinal and higher roll mode time constant in lateral, the flying qualities for high angle of attack aircraft get better. Therefore, the developed criteria is more adaptable in evaluation the flying qualities for the high angle of attack aircraft. This new criteria could be used as a guideline when designing modern air fighters.
- high angle of attack /
- flying qualities /
- criteria for evaluation /
- mission-oriented /
- air fighter

HTML全文

参考文献(16)

[1]	张翔伦,左玲,杨蔷薇.基于机动动作链的飞行品质评价方法研究[J].飞行力学,2006,24(3):13-16.Zhang X L,Zuo L,Yang Q W.Research on the maneuvers-based flying qualities evaluation method[J].Flying Dynamics,2006,24(3):13-16(in Chinese).
[2]	方振平,陈万春,张曙光.航空飞行器飞行动力学[M].北京:北京航空航天大学出版社,2005:196-204.Fang Z P,Chen W C,Zhang S G.Flying dynamics of aircraft[M].Beijing:Beihang University Press,2005:196-204(in Chinese).
[3]	Krekeler G,Wilson D,Riley D.High angle of attack flying qualities criteria,AIAA-1990-0219 [R].Reston:AIAA,1990.
[4]	Wilson D J,Citurs K D,Davidson J B.Development of flying qualities criteria for 60° angle of attack,AIAA-1994-3506-CP[R].Reston:AIAA,1994.
[5]	董彦飞,荣康,高杰.飞机飞行品质规范发展综述[J].飞行力学,2010,28(5):1-4.Dong Y F,Rong K,Gao J.Development of aircraft flying qualities specification[J].Flying Dynamics,2010,28(5):1-4(in Chinese).
[6]	Wilson D J,Riley D R,Citurs K D.Aircraft maneuvers for the evaluation of flying qualities and agilit.VOL2:Maneuver descriptions and selection guide,WL-TR-93-3082[R].St.Louis:WL-TR,1993.
[7]	冯亚昌,高金源,李陆豫.飞机飞行品质[M].北京:国防工业出版社,2003:54-59.Feng Y C,Gao J Y,Li L Y.Aircraft handling qualities[M].Beijing:National Defense Industry Press,2003:54-59(in Chiniese).
[8]	MIL-STD-1797A Military standard:Flying qualities of piloted aircraft[S].Washington D.C.:Department of Defense,1997:39-44.
[9]	MIL-F-8785C Military specification:Flying qualities of piloted airplanes[S].Washington D.C.:Department of Defense,1980:189-193.
[10]	Mitchell G D,Klyde D H.A set of demonstration maneuvers for the evaluation of aircraft handling qualities,STI ITR-1310-1[R].St.Louis:STI ITR,1996.
[11]	李淼,王立新,黄成涛.舵面特性对飞翼构型作战飞机短周期品质的影响[J].航空学报,2009,30(11):2059-2065.Li M,Wang L X,Huang C T.Influence of control surface characteristics on short period mode flying qualities for flying wing aircraft[J].Acta Aeronautica et Astronautica Sinica,2009,30(11):2059-2065(in Chinese).
[12]	Mitchell D G,Roger H H,Bimal L A,et al.Proposed incorporation of mission-oriented flying qualities into MIL-STD-1797A,WL-TR-94-3162[R].St.Louis:WL-TR,1994.
[13]	邓以高.飞行器姿态控制方法综述[J].战术导弹控制技术,2006,53(2):9-13.Deng Y G.Summarization of air vehicle's attitude control methods[J].Control Technology of Missile,2006,53(2):9-13(in Chinese).
[14]	黄华,徐幼平,邓志武.基于Flightgear模拟器的实时可视化飞行仿真系统[J].系统仿真学报,2007,19(19):4421-4423.Huang H,Xu Y P,Deng Z W.Real-time visual flight simulation system based on Flightgear simulator[J].Journal of System Simulation,2007,19(19):4421-4423(in Chinese).
[15]	王美仙,李明,张子军.飞行器控制律设计方法发展综述[J].飞行力学,2007,25(2):1-4.Wang M X,Li M,Zhang Z J.Developing status of control law design methods for flight[J].Flying Dynamics,2007,25(2):1-4(in Chinese).
[16]	龙晋伟,潘文俊,王立新.战斗机动态逆控制律对比研究[J].飞行力学,2013,31(4):297-300.Long J W,Pan W J,Wang L X.A comparison of nonlinear dynamics inversion control designs for an fighter aircraft[J].Flying Dynamics,2013,31(4):297-300(in Chinese).