Advanced Search
Volume 30 Issue 06
Jun.  2004
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2004  >  30(06): 561-564.
Yu Zhongjun, Zhao Jingquan. Simulation on pressure regulator characteristic[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(11): 1379-1383. (in Chinese)
Citation: He Heng, Wu Ruixiang. Improved BP neural network in design of aircraft antiskid braking system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(06): 561-564. (in Chinese)
shu

Improved BP neural network in design of aircraft antiskid braking system

  • School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 22 Jan 2003
  • Publish Date: 30 Jun 2004
    Abstract
  • The construction of Sp (perfect slip ratio) identifier with back-propagation neural network was proposed to prevent skidding and have the best braking effect in the aircraft braking process. In order to improve the learning ability of the network, a type of self-adaptive learning rate method, second-order learning rate method, was introduced. Some problems in the practice of this method were discussed and the solutions were presented. A third-order learning rate method was deduced based on the method. The method of reasonable configuration of active functions was proposed. The combination of these methods renders better learning precision and speed.

     

    • FullText(HTML)
    • References(1)
  • [1] 焦志强. 系缆气球气动力、动稳定性及大气扰动响应 . 北京:北京航空航天大学航空科学与工程学院,2003 Jiao Zhiqiang. Aerodynamic estimation stability and dynamics repouse for a tethered balloon .BeiJing:School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics,2003 [2] Jones S P,DeLaurier J D. Aerodynamic estimation techniques for aerostats and airships . AIAA-81-1339,1981 [3]Jones S P. Aerodynamics of a new aerostat design with inverted-y fins . AIAA 85-0867-CP, 1985
    • Relative Articles

  • Relative Articles

    [1]LI Huan, CUI Pengcheng, JIA Hongyin, GONG Xiaoquan, WU Xiaojun. Numerical Simulation of TSTO Interstage Separation Considering Constraint Force[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0839
    [2]ZHOU Y J，WAN Q，XU Y Z，et al. Redundancy design of a FADS system on a complex leading-edge vehicle using neural network approach[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（3）：757-764 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0341.
    [3]XIAO L F，ZHOU L W，LI X D. Numerical simulation of deformed airfoil modal after blast shock wave[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：341-349 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0244.
    [4]LI C Q，ZHAN Y Q，WANG Z M，et al. Numerical simulation of iliac vein compression syndrome in hemodynamics[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2646-2654 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0693.
    [5]LEI J M，WU Z X，XIE W Y. Numerical simulation investigation on water surface skipping motion characteristics of sea-skimming projectile[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：2975-2983 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0813.
    [6]CHEN B，LUO L，JIANG A L，et al. Numerical simulation of separation characteristics for internally buried weapon at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2113-2122 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0627.
    [7]ZHANG P H，CHEN H Y，ZHANG J，et al. Passive flow control for weapon bay at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2913-2920 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0790.
    [8]GAO J C，CHEN W J，HU W J，et al. Analysis of CO2 distribution characteristics in cabin of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2510-2517 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0683.
    [9]ZHANG P H，CHENG X H，CHEN H Y，et al. Unsteady flow mechanism of high Mach number cavity[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1940-1947 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0609.
    [10]HE Z P，ZHOU J X，XIN J，et al. Unsteady flow characteristics of turbine rotor passage under rim seal effect[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：273-283 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0223.
    [11]ZHANG Pei-hong, JIA Hong-yin, ZHAO Jiao, WU Xiao-jun, ZHOU Gui-yu, ZHANG Yao-bing. Numerical simulation research on opposing jet interaction characteristics of rocket inverse flight[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0710
    [12]LIU J，LIU H，YANG J L. Collapse modes and energy absorption performance of conventional and re-entrant hexagonal tubes under lateral compression[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2021-2028 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0623.
    [13]XIE N，TANG Y M，ZHANG Y，et al. Numerical study of blood pump weaning effects on hemocompatibility of centrifugal blood pump[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1680-1688 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0494.
    [14]ZHANG P H，TANG Y，TANG J，et al. Simulation of cavity flow at high Mach number based on adaptive unstructured hybrid mesh[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1311-1318 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0424.
    [15]HAN Y F，HU X S，GAO Y，et al. Comparison of turbulence models for unsteady flow simulation in a long and narrow cabin[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：957-964 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0335.
    [16]PENG L，LI L，ZHAO W. Numerical study on coupled heat transfer of rotating disc in centrifugal atomization[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3456-3466 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0152.
    [17]WANG Weiqi, XING Yuming, ZHENG Wenyuan, HAO Zhaolong. Phase change heat transfer characteristics and fractal optimization of radial plate fin tube[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2520-2528. doi: 10.13700/j.bh.1001-5965.2021.0140
    [18]GUO Qi, SHEN Xiaobin, LIN Guiping, ZHANG Shijuan. Numerical simulation of icing on aircraft rotating surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2259-2269. doi: 10.13700/j.bh.1001-5965.2021.0081
    [19]WENG Huiyan, CAI Guobiao, ZHENG Hongru, LIU Lihui, ZHANG Baiyi, HE Bijiao. Numerical simulation of effect of background pressure on electric propulsion plume field[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1854-1862. doi: 10.13700/j.bh.1001-5965.2021.0039
    [20]ZHANG Chao, LIU Jianchun, FANG Xin. Damage analysis in composite laminates under low velocity oblique impact[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2388-2397. doi: 10.13700/j.bh.1001-5965.2021.0154
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(864) PDF downloads(4) Cited by()
    Proportional views
    Related

    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.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return