Advanced Search
Volume 42 Issue 10
Oct.  2016
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(10): 2222-2230.
MENG Xiangguang, WANG Lixin, LIU Hailianget al. Mathematical simulation and assessment of airworthiness compliance of climb gradient during takeoff of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(10): 2222-2230. doi: 10.13700/j.bh.1001-5965.2015.0617(in Chinese)
Citation: MENG Xiangguang, WANG Lixin, LIU Hailianget al. Mathematical simulation and assessment of airworthiness compliance of climb gradient during takeoff of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(10): 2222-2230. doi: 10.13700/j.bh.1001-5965.2015.0617(in Chinese)
shu

Mathematical simulation and assessment of airworthiness compliance of climb gradient during takeoff of civil aircraft

doi: 10.13700/j.bh.1001-5965.2015.0617
  • 1.

    Large Aircraft Advanced Training Center, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

Funds:  National High-tech Research and Development Program of China (2014AA110501)
  • Received Date: 22 Sep 2015
  • Publish Date: 20 Oct 2016
    Abstract
  • The climb gradient along the takeoff path reflects the civil aircraft's ability of flying over the ground obstacles to reach the safe height. According to the requirements of airworthiness regulations for takeoff procedure and climb performance, an airworthiness compliance assessment method of climb gradient with one engine inoperative was proposed based on the pilot-in-loop flight simulation and calculation. A nonlinear aircraft model, a landing gear model and pilot control models were established and assessment criteria were set up. A simulation task of takeoff with one engine inoperative as well as the control procedure of the pilot was designed. The climb gradient of various states was assessed based on the closed-loop digital flight simulation. This method can be applied to the preliminary design phase of civil aircrafts to provide support for the configuration design and the determination of takeoff weight limit, and offer theoretical references for flight tests of climb performance with one engine inoperative.

     

    • FullText(HTML)
  • loading
    • References(19)
  • [1]
    黄太平.飞机性能工程[M].北京:科学出版社,2005:37-43.HUANG T P.Aircraft performance engineering[M].Beijing:Science Press,2005:37-43(in Chinese).
    [2]
    李旭,臧志恒,魏志强.民用飞机起飞第2爬升段爬升梯度计算分析[J].交通与计算机,2006,24(5):85-87.LI X,ZANG Z H,WEI Z Q.Climb gradient calculation for the second segment in airplane takeoff[J].Computer and Communications,2006,24(5):85-87(in Chinese).
    [3]
    JOHNSON S C,GLOVER H.Method for determining a currently obtainable climb gradient of an aircraft:U.S.Patent 6,691,004[P].2004-02-10.
    [4]
    FILIPPONE A.Theoretical framework for the simulation of transport aircraft flight[J].Journal of Aircraft,2010,47(5):1679-1696.
    [5]
    韩丰波,于新江,樊丹.某大型运输机不对称推力飞行初探[J].飞行力学,1997,15(3):82-85.HAN F B,YU X J,FAN D.Discussion on non-symmetric thrust flight for a certain type of the large transporter[J].Flight Dynamics,1997,15(3):82-85(in Chinese).
    [6]
    中国民用航空局.中国民用航空规章第25部:运输类飞机适航标准:CCAR-25R4[S].北京:中国民用航空局,2011.Civil Aviation Administration of China.China civil aviation regulations part 25:Airworthiness standards of transport category aircraft:CCAR-25R4[S].Beijing:Civil Aviation Administration of China,2011(in Chinese).
    [7]
    ETKIN B.Dynamics of flight:Stability and control[M].New York:John Wiley & Sons,1995.
    [8]
    刘海良,王立新.基于数字虚拟飞行的民用飞机纵向地面操稳特性评估[J].航空学报,2015,36(5):1432-1441.LIU H L,WANG L X.Assessment of longitudinal ground stability and control for civil transport aircraft based on virtual flight testing methodology[J].Acta Aeronautica et Astronautica Sinica,2015,36(5):1432-1441(in Chinese).
    [9]
    PI W S,YAMANE J R,SMITH M J C.Generic aircraft ground operation simulation:AIAA-1986-0989[R].Reston:AIAA,1986.
    [10]
    KHAPANE P D.Simulation of asymmetric landing and typical ground maneuvers for large transport aircraft[J].Aerospace Science and Technology,2003,7(8):611-619.
    [11]
    SMILEY R F,HORNE W B.Mechanical properties of pneumatic tires with special reference to modern aircraft tires:NASA TR-64[R].Hampton:NASA,1960.
    [12]
    WOOD G,BLUNDELL M,SHARMA S.A low parameter tyre model for aircraft ground dynamic simulation[J].Materials & Design,2012,35:820-832.
    [13]
    贾重任,黄成涛,王立新.空中最小操纵速度的人机闭环数学仿真计算[J].北京航空航天大学学报,2013,39(5):580-584.JIA Z R,HUANG C T,WANG L X.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).
    [14]
    LIU F,WANG L,TAN X.Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM[J].Chinese Journal of Aeronautics,2015,28(1):112-120.
    [15]
    HOSMAN R,VAN DER GEEST P,VAN DER ZEE J.Development of a pilot model for the manual balked landing maneuver:AIAA-2009-5818[R].Reston:AIAA,2009.
    [16]
    POOL D M,ZAAL P M T,DAMVELD H J,et al.Pilot equation in manual control of aircraft dynamics[C]//Proceedings of the 2009 IEEE International Conference on Systems,Man,and Cybernetics.San Antonio:[s.n.],2009.
    [17]
    ROBINSON J,BARNES S,WEBB M,et al.The use of pilot modeling in aviation regulatory affairs:AIAA-2009-5825[R].Reston:AIAA,2009.
    [18]
    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,2003:139-142.GAO J Y,LI L Y,FENG Y C,et al.Aircraft handling qualities[M].Beijing:National Defend Industry Press,2003:139-142(in Chinese).
    [19]
    OHME P.A model-based approach to aircraft takeoff and landing performance assessment:AIAA-2009-6154[R].Reston:AIAA,2009.
    • Relative Articles
    • 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(854) PDF downloads(702) 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