Advanced Search
Volume 39 Issue 5
May  2013
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(5): 580-584.
Qian Huaming, Jiang Bo. Method base on multi-channel satellite cloud image for typhoon segmentation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 466-471. (in Chinese)
Citation: Jia Zhongren, Huang Chengtao, Wang Lixinet al. Mathematical simulation method to calculate air minimum control speed[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 580-584. (in Chinese)
shu

Mathematical simulation method to calculate air minimum control speed

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 10 May 2012
  • Rev Recd Date: 26 Nov 2012
  • Publish Date: 31 May 2013
    Abstract
  • The determination of the air minimum control speed VMC is an important content in the civil aircraft airworthiness compliance verification. The value of VMC is one of the vital bases to design the rudder and engine layout of an aircraft. Based on the physical understanding of the VMC airworthiness compliance flight test, a method to calculate VMC by mathematical simulation was proposed. According to the behavior characteristics of the pilot in the VMC flight test, the mathematical pilot model was established. Then, the pilot-aircraft closed loop flight simulation model for the VMC flight test was set up. Based on the accurate mathematical simulation of the VMC flight test, the value of VMC under different test conditions can be obtained. The method to calculate VMC proposed has important theoretical and practical value to guide the aircraft design and airworthiness compliance flight test.

     

    • FullText(HTML)
    • References(12)
  • [1]
    CCAR-25-R3 运输类飞机适航标准[S]
    CCAR-25-R3 Airworthiness standards:transport category airplanes[S] (in Chinese)
    [2]
    Ohme P.A model-based approach to aircraft takeoff and landing performance assessment[J].AIAA 2009-6154,2009
    [3]
    Filippone A.Theoretical framework for the simulation of transport aircraft flight[J].Journal of Aircraft,2010,47(5):1679-1696
    [4]
    张立彬,李宗娟,曹东波.不对称推力飞行的最小操纵速度分析[J].飞行力学,2000,18(1):61-63
    Zhang Libin,Li Zongjuan,Cao Dongpo.Research into minimum control speed at the non-symmetric thrust flight[J].Flight Dynamics,2000,18(1):61-63(in Chinese)
    [5]
    Phillips W F,Niewoehner R J.Effect of propeller torque on minimum-control airspeed[J].Journal of Aircraft,2006,43(5):1393-1398
    [6]
    肖业伦,金长江.大气扰动中的飞行原理[M].北京:国防工业出版社,1993:77-81
    Xiao Yelun,Jin Changjiang.Flight principle in the atmospheric perturbation[M].Beijing:National Defense Industry Press,1993:77-81(in Chinese)
    [7]
    陈永亮.飞机大迎角非线性动力学特性分析与控制[D].南京:南京航空航天大学航空宇航学院,2007
    Chen Yongliang.Nonlinear dynamic characteristics analysis and control of aircraft at high-angle-of-attack[D].Nanjing:College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,2007(in Chinese)
    [8]
    杨翠霞,程伟豪,张培田,等.民机地面最小操纵速度试飞技术研究[J].飞行力学,2007,25(3):75-78
    Yang Cuixia,Cheng Weihao,Zhang Peitian,et al.Flight test technology research on ground minimum control speed of civil airplanes[J].Flight Dynamics,2007,25(3):75-78(in Chinese)
    [9]
    黄成涛,王立新.风雨对飞机飞行安全性的影响[J].航空学报,2010,31(4):694-700
    Huang Chengtao,Wang Lixin.Effects of rain and wind on aircraft flight safety[J].Acta Aeronautica et Astronautica Sinica,2010,31(4):694-700(in Chinese)
    [10]
    高浩,朱培申,高正红.高等飞行动力学[M].北京:国防工业出版社,2004:222-223
    Gao Hao,Zhu Peishen,Gao Zhenghong.Advanced flight dynamics[M].Beijing:National Defense Industry Press,2003:222-223(in Chinese)
    [11]
    Huang Chengtao,Wang Lixin,Jia Zhongren.A method to calculate the aircraft ground minimum control speed based on mathematical simulation[J].Procedia Engineering,2011,17:24-38
    [12]
    金镭,刘友丹.飞机地面最小操纵速度要求浅析[J].航空标准化与质量,2003(233):27-30
    Jin Lei,Liu Youdan.A discussion of aircraft ground minmum control speed[J].Aeronautic Standardization & Quality,2003(233):27-30(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]LIU Y S，YANG Y X，LIU Y，et al. Gust alleviation control system of flexible aircraft considering rudder efficiency[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：248-256 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0952.
    [2]WEI Kun-yu, LI Chen-di, LI Bo-wen, YUAN Yuan, HE Xiao-fan. Research on Developing Design Gust Load Spectrum for Bomber-Mounted Air-to-Ground Missiles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0126
    [3]CHEN P X，WU C C，NI Z Y. Dynamic modelling and simulation of a tethered-net in space[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2951-2962 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0747.
    [4]LI Bowen, LEI Xiaoyong. Flight task recognition and action segmentation based on SVM[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0635
    [5]JIANG Y H，GUO T，GONG Q，et al. Analysis and modeling method of civil aircraft emergency scenario[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（3）：839-849 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0339.
    [6]ZHANG Jun, HUANG Minghui, WANG Yuelin, YANG Xing, YE Min, JIA Yongle. Unmanned trajectory tracking strategy for aircraft tug with MPC method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023-0431
    [7]SHE W Q，LIU Y B，CHEN B Y. Altitude control strategy for high-aspect-ratio wings with active morphing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1746-1752 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0612.
    [8]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.
    [9]ZHOU D P，LI H Q，WANG Y G，et al. Aircraft system identification algorithm based on generalized equivalent model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1454-1462 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0507.
    [10]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
    [11]LYU Yuzhu. Study on Flight Characteristics and Speed Limit of Helicopter with Slung Load[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0563
    [12]JIN Z B，LI D C，SUN Y，et al. Man-machine cooperative control of helicopter and flight experimental validation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3022-3030 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0038.
    [13]FENG W C，ZHANG T，LI W. Experimental study on adverse attitude emergency evacuation of civil aircraft after crash landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1553-1562 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0483.
    [14]CUI K K，HAN W，LIU Y J，et al. Automatic wave-off control algorithm for carrier aircraft based on DM-DSC[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：900-912 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0362.
    [15]YAN Y，MA X L. Air freight route planning based on transshipment under air alliance[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：115-127 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0166.
    [16]SHI Y，WAN Z Q，WU Z G，et al. Aerodynamic order reduction method for elastic aircraft flight dynamics simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1689-1706 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0510.
    [17]WANG Shaoping, CHEN Rentong, ZHANG Chao. Reliability estimation for aircraft hydraulic pump based on bivariate performance degradation analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1613-1623. doi: 10.13700/j.bh.1001-5965.2022.0297
    [18]GONG Xiao, HUANG Jinguo, CHEN Hongyu, WANG Tianmiao, LIANG Jianhong. Dynamics modeling and kinematics calculation of webbed-feet during cormorant's take-off[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(10): 2096-2105. doi: 10.13700/j.bh.1001-5965.2018.0030
    [19]LIU Chuankai, LI Yanru. Performance simulation model of millimeter-scale micro turbine engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(7): 1430-1437. doi: 10.13700/j.bh.1001-5965.2017.0566
    [20]CUI Jianguo, XU Lingyu, YU Mingyue, JIANG Liying, WANG Jinglin, LIN Zeli. Health state prediction technique for aircraft wing based on MEMD and ELM[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(8): 1501-1508. doi: 10.13700/j.bh.1001-5965.2016.0610
    • 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(2304) PDF downloads(835) 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