| Citation: | Chai Xue, Wang Ganglin, Wu Zheet al. Aileron control and reconfiguration of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1511-1515. (in Chinese)
|
|
[1] Moody L A.The history and future of flight control simulation .AIAA-2004-5149,2004 [2] 杨伟.容错飞行控制系统[M].西安:西北工业大学出版社,2007:107-114 Yang Wei.Fault tolerance flying control system [M].Xi-an: Northwestern Polytechnic University Press,2007:107-114(in Chinese) [3] 马松辉, 吴成富, 陈怀民.飞翼飞机稳定性与操纵性研究[J].飞行力学,2006,24(3): 17-23 Ma Songhui, Wu Chengfu, Chen Huaimin. Study on stability and maneuverability of flying wing aircraft [J].Flight Dynamics,2006,24(3): 17-23(in Chinese) [4] Burken J J. Reconfigurable flight control designs with application to the X-33 vehicle .AIAA-99-4134, 1999 [5] 冯巧玲.自动控制原理[M].北京:北京航空航天大学出版社, 2003:67-71 Feng Qiaoling. Automatic control theory [M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2003: 67-71(in Chinese) [6] 吴森堂,费玉华.飞行控制系统[M].北京:北京航空航天大学出版社,2005: 52-79 Wu Sentang, Fei Yuhua. Aircraft control system [M].Beijing: Beijing University of Aeronautics and Astronautics Press,2005: 52-79(in Chinese) [7] Esteban S. Static and dynamic analysis of an unconventional plane: flying wing .AIAA-2001-4010, 2001 [8] 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 Li Lin,Ma Chao, Wang Lixin. Lateral-directional control characteristics of high aspect-ratio flying wing configurations [J]. Beijing: Journal of Beijing University of Aeronautics and Astronautics, 2007,33(10):1186-1190(in Chinese) [9] 王青,孙蕊.基于特征结构配置的导弹可重构控制器设计[J].北京:北京航空航天大学学报,2008,34(3):304-306 Wang Qing, Sun Rui.Reconfigurable controller design for missile using eigen structure assignments [J].Beijing: Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(3):304-306(in Chinese) [10] Tournes C, Shtessel Y B. Sliding mode control for tailless aircraft .AIAA-97-3633, 1997 [11] Dmitriev V G,Shkadov L M,Denisov V E,et al.The flying-wing concept-chances and risks .AIAA-2003-2887,2003 [12] Davidson R W.Flight control design and test of the joint unmanned combat air system(J-UCAS) X-45A .AIAA-2004-6557,2004
|
| [1] | TIAN D K，ZHANG J W，JIN L，et al. Design and analysis of morphing wing mechanism based on equilateral Bennett mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：742-752 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0139. |
| [2] | HU YaoWei, SHANG YunBin, HE Xi, YIN JinTao, JIANG ShengJu, LEI JuanMian. Wind Tunnel Experiment and Numerical Simulation on the Magnus Effect of Rotating Wing-body Combination[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0830 |
| [3] | XU Tao, SUN Youchao, LI Longbiao, HU Yu. Dynamic Reconfiguration Strategy for IMA Based on Fault Propagation Modeling[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0422 |
| [4] | HU Gengshuo, JIAO Jian, HU Langxiao, JING Yongfeng. Reliability modeling and evaluation method of IMA under dynamic reconfiguration[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0188 |
| [5] | CHENG Y，QIU B W，YU L，et al. Influence of maneuvering modes on flared landing performance of parafoil system[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3940-3946 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0914. |
| [6] | YUAN Y，LIU J，YU J Q，et al. Aerodynamic layout optimization design of high-speed folding-wing vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3410-3416 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0849. |
| [7] | WANG Xiaoliang, WANG Congsheng, SHI Yuxiang, HE Weikun. The Classification Method of Multirotor Drones and Flying Birds under Low Signal-to-Noise Ratio for Radar[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0585 |
| [8] | SONG Ziyi, LI Yanjun, YU Li, LI Xixi. Coupling model analysis for aerodynamic performance of parafoil with maneuvers[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0558 |
| [9] | WANG Y T，LAN Q S，ZHOU Z，et al. Design and aerodynamic analysis of blended wing body with variable camber technology[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1292-1307 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0493. |
| [10] | XU H，HAN J L，CHEN Y，et al. Thickness correction by lifting surface method and its application in morphing simulation of folding wing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3806-3814 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0926. |
| [11] | KONG Lingwei, LI Weiqi. Optimization of aircraft speed vector control based on Hp adaptive Pseudo-spectral method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0405 |
| [12] | FENG Yu-xuan, HUO Ying-yuan, LI Jun-jie. Design of multiple-input/multiple-output control law for active flutter suppression of flying-wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0144 |
| [13] | XU H，HAN J L，XI Y，et al. Aeroelastic morphing flight simulation platform for a folding wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1921-1930 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0536. |
| [14] | Zhang Wei, Zhou Lin, Chen Xian, Shu Bowen, Huang Jiangtao, Gao Zhenghong. Sensitivity analysis and optimization design of high stealth flying wing layout airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0112 |
| [15] | WANG X Q，LAI F L，ZHAO C L. Reconfiguration control and motion simulation of tilt-rotor aircraft with multilinks[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1523-1531 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0522. |
| [16] | WANG L N，LIU Z B，YUAN J B，et al. Adaptive fault diagnosis and estimation for quadrotor UAV[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2395-2405 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0656. |
| [17] | WANG R C，ZHANG G X，WANG X Y，et al. Aerodynamic performance analysis of supercritical airfoil with lower surface jet[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1671-1679 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0489. |
| [18] | YANG K L，HAN D. Influence of rotor/wing aerodynamic interference on performance of compound helicopters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1761-1771 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0561. |
| [19] | CHENG Yi, ZHAO Jin-rui, HUANG Shui-lin, YU Zhi-hao, DENG Xu-dong. Research on dynamic characteristics of distributed multi-rotor/tilting wing aeroelastic coupling[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0253 |
| [20] | WANG Y W，LEI R W，WANG H. Structural topology optimization of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：482-490 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0262. |
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.
Chai Xue, Wang Ganglin, Wu Zheet al. Aileron control and reconfiguration of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1511-1515. (in Chinese)
DownLoad: