| Citation: | CONG Bin, WANG Lixin. Crosswind take-off and landing characteristics of flying wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(5): 1023-1030. doi: 10.13700/j.bh.1001-5965.2016.0458(in Chinese)
|
The stability and controllability characteristics of flying wings are much different from those of conventional airplanes. This difference is prevalent in crosswind take-off and landing. To ensure flight safety in these circumstances, this paper conducts calculation and analysis of trim and response characteristics in crosswind take-off and landing for flying wings. From these, the differences between flying wings and conventional airplanes are derived, with the conclusion that the roll-over is the most serious problem for flying wings taking off or landing in crosswinds. The control efficiency requirements of innovative control surfaces on flying wings during take-off and landing are analyzed based on the control surfaces' control and usability characteristics. Two control strategies commonly applied to flight in crosswind conditions are simulated and compared; a suitable one for flying wings is proposed.
| [1] |
高金源, 李陆豫, 冯亚昌, 等.飞机飞行品质[M].北京:国防工业出版社, 2003:261-264.
GAO J Y, LI L Y, FENG Y C, et al.Aircraft flying qualities[M].Beijing:National Defense Industry Press, 2003:261-264(in Chinese).
|
| [2] |
FOSTER T M, BOWMAN W J.Dynamic stability and handling qualities of small unmanned-aerial-vehicles:AIAA-2005-1023 [R].Reston:AIAA, 2005.
|
| [3] |
马超, 王立新.飞翼布局作战飞机起降特性分析[J].北京航空航天大学学报, 2009, 35(4):429-433.
MA C, WANG L X.Take-off and landing features of flying-wing configuration fighter[J].Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(4):429-433(in Chinese).
|
| [4] |
李林, 马超, 王立新.大展弦比飞翼构型的横航向操纵特性[J].北京航空航天大学学报, 2007, 33(10):1186-1190. doi: 10.3969/j.issn.1001-5965.2007.10.014
LI L, MA C, WANG L X.Lateral-directional control characteristics of high aspect-ratio flying wings configurations[J].Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10):1186-1190(in Chinese). doi: 10.3969/j.issn.1001-5965.2007.10.014
|
| [5] |
王艳丽, 周洲, 张琳.飞翼无人机侧风着陆控制方法研究[J].飞行力学, 2009, 27(1):24-26.
WANG Y L, ZHOU Z, ZHANG L.Flying wing UAV crosswind landing control mothed[J].Flight Dynamics, 2009, 27(1):24-26(in Chinese).
|
| [6] |
王磊, 王立新, 贾重任.飞翼布局飞机开裂式方向舵作用特性和使用特点[J].航空学报, 2011, 32(8):1392-1399. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201108003.htm
WANG L, WANG L X, JIA Z R.Control features and application characteristics of split drag rudder utilized by flying wing[J].Acta Aeronautica et Astronautica Sinica, 2011, 32(8):1392-1399(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201108003.htm
|
| [7] |
MA C, WANG L X.Flying-wing aircraft control allocation[C]//Proceedings of 47th AIAA Aerospace Sciences Meeting and Exhibit.Reston: AIAA, 2009.
|
| [8] |
马超, 李林, 王立新.大展弦比飞翼布局飞机新型操纵面设计[J].北京航空航天大学学报, 2007, 33(2):149-153.
MA C, LI L, WANG L X.Design of innovative control surfaces of flying wing aircrafts with large ratio aspect[J].Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(2):149-153(in Chinese).
|
| [9] |
马亭亮.侧风对飞机起飞着陆的影响及修正原理[J].技术研发, 2013, 20(13):66-67. http://www.cnki.com.cn/Article/CJFDTOTAL-JSYS201311038.htm
MA T L.Research on influences of crosswind and modification methods during take-off and landing period[J].Technology and Market, 2013, 20(13):66-67(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JSYS201311038.htm
|
| [10] |
张立彬, 苏胜昔.关于飞机侧风着陆问题的分析[J].飞行力学, 2002, 20(4):51-55. http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX200204012.htm
ZHANG L B, SU S X.Analysis to the problem of airplane's cross-wind landing[J].Flight Dynamics, 2002, 20(4):51-55(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX200204012.htm
|
| [11] |
宋辉, 陈欣, 李春涛.大展弦比无人机抗侧风着陆控制研究[J].飞行力学, 2011, 29(6):26-30. http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201106007.htm
SONG H, CHEN X, LI C T.Research on automatic landing control for high span-chord ratio UAV in crosswind[J].Flight Dynamics, 2011, 29(6):26-30(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201106007.htm
|
| [12] |
嵇鼎毅, 陆宇平.飞翼布局无人机抗侧风自动着陆控制[J].飞机设计, 2011, 29(6):25-28.
JI D Y, LU Y P.Automatic crosswind landing control for umnanned air vehicles with a flying wing configuration[J].Aircraft Design, 2011, 29(6):25-28(in Chinese).
|
| [13] |
王鹏, 马松辉, 陈怀民.飞翼无人机着陆过程中的抗侧风控制研究[J].计算机仿真, 2007, 26(12):78-81. http://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200912026.htm
WANG P, MA S H, CHEN H M.Research on counteracting side wind in landing control for fly-wing UAV[J].Computer Simulation, 2007, 26(12):78-81(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200912026.htm
|
| [14] |
马超, 李林, 王立新.小展弦比飞翼布局作战飞机可控性设计方法[J].航空学报, 2008, 29(4):788-794. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB200804005.htm
MA C, LI L, WANG L X.Design method of controllability of low aspect-ratio flying wing configuration combat aircraft[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(4):788-794(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB200804005.htm
|
| [15] |
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, 2005:206.
FANG Z P, CHEN W C, ZHANG S G.Aircraft flight dynamics[M].Beijing: Beihang University Press, 2005:206(in Chinese).
|
| 1. | 刘柳，向先宏，张宇飞，陈海昕，魏闯，朱剑，杨普. 一种高升阻比非常规翼身融合燕尾气动布局. 航空学报. 2024(06): 96-109 .  | |
| 2. | 丛斌，孟祥瑞，张迪. 飞翼飞机新型操纵舵面故障效能影响分析. 战术导弹技术. 2020(02): 29-33 . |
Figures(5) / Tables(6)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
CONG Bin, WANG Lixin. Crosswind take-off and landing characteristics of flying wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(5): 1023-1030. doi: 10.13700/j.bh.1001-5965.2016.0458(in Chinese)
DownLoad:
