留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

民机横航向静稳定性适航符合性数学仿真评估

陈俊平 王立新

陈俊平, 王立新. 民机横航向静稳定性适航符合性数学仿真评估[J]. 北京航空航天大学学报, 2017, 43(2): 301-310. doi: 10.13700/j.bh.1001-5965.2016.0119
引用本文: 陈俊平, 王立新. 民机横航向静稳定性适航符合性数学仿真评估[J]. 北京航空航天大学学报, 2017, 43(2): 301-310. doi: 10.13700/j.bh.1001-5965.2016.0119
CHEN Junping, WANG Lixin. Mathematical simulation and evaluation for lateral-directional static stability airworthiness compliance of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2): 301-310. doi: 10.13700/j.bh.1001-5965.2016.0119(in Chinese)
Citation: CHEN Junping, WANG Lixin. Mathematical simulation and evaluation for lateral-directional static stability airworthiness compliance of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2): 301-310. doi: 10.13700/j.bh.1001-5965.2016.0119(in Chinese)

民机横航向静稳定性适航符合性数学仿真评估

doi: 10.13700/j.bh.1001-5965.2016.0119
基金项目: 

国家“863”计划 2014AA110501

详细信息
    作者简介:

    陈俊平,男,博士研究生。主要研究方向:飞机设计、飞行安全

    王立新,男,教授,博士生导师。主要研究方向:飞机设计、飞行动力学与控制、飞行安全等

    通讯作者:

    王立新,E-mail:wlx_c818@163.com

  • 中图分类号: V212.12

Mathematical simulation and evaluation for lateral-directional static stability airworthiness compliance of civil aircraft

Funds: 

National High-tech Research and Development Program of China 2014AA110501

More Information
  • 摘要:

    针对适航标准对民机横航向静稳定性的要求,提出了一种基于人机闭环数学仿真计算的适航符合性评估方法。根据适航条款的要求提出了量化评估指标,建立了飞机系统模型和驾驶员操纵模型,以实现定常直线侧滑飞行等的特定飞行任务的人机闭环数学仿真,并依据数学仿真结果和评估指标对飞机的横航向静稳定性做出评估。运用此方法完成了某型民机设计方案的适航符合性评估,并较准确地确定了飞机横航向2个静稳定导数的合理取值范围。该方法可应用于民机的概念方案设计,计算结果可为飞行试验提供理论参考。

     

  • 图 1  方向舵指令

    δre—方向舵偏度指令。

    Figure 1.  Rudder command

    图 2  人机闭环系统结构图

    YPV—驾驶员操纵速度模型;YPγ—驾驶员操纵航迹倾角模型;YPθ—驾驶员操纵俯仰角模型;—驾驶员操纵航迹偏角角速率模型;YPϕ—驾驶员操纵滚转角模型;YPδr—驾驶员操纵方向舵模型;θ—俯仰角。

    Figure 2.  Man-machine closed-loop system structure diagram

    图 3  Hosman驾驶员模型

    θerr—俯仰角误差;ϕerr—滚转角误差;Hpn—McRuer模型回路;Hpm—驾驶员加速度感受回路;Hec—无时间延迟的McRuer模型;τn—驾驶员信息反应时延;Hnm—驾驶员人体肌肉动作延迟模型;δec—升降舵偏大指令;δac—副翼偏度指令;—滚转角角加速度;—俯仰角角加速度;Hscc—人体内耳前庭器官的半规管模型;km—驾驶员运动感官增益;τm—驾驶员运动神经延迟。

    Figure 3.  Hosman pilot model

    图 4  仿真流程

    Figure 4.  Simulation procedure

    图 5  横航向静稳定性评估仿真结果

    Figure 5.  Simulation results of lateral-directional static stability evaluation

    图 6  正比关系验证

    Figure 6.  Proportional relationship validation

    图 7  C范围确定

    Figure 7.  Range determination of C

    图 8  C和|C|的可行域

    Figure 8.  Feasible region of C and |C|

    图 9  副翼饱和的横航向静稳定性评估仿真结果

    Figure 9.  Simulation results of lateral-directional static stability evaluation with aileron saturation

    表  1  驾驶员模型参数取值范围

    Table  1.   Range of pilot model parameters

    驾驶员参数 取值范围
    kx [1, 100]
    Tx (0, 1.0] s
    τx [0.06, 0.30] s
    下载: 导出CSV
  • [1] 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,2005:260-262.

    FANG Z P,CHEN W C,ZHANG S G.Flight dynamics of aerospace aircraft[M].Beijing:Beihang University Press,2005:260-262(in Chinese).
    [2] IORIO C,NAPOLITANO M R,SEANOR B A,et al.Parameter estimation for the NASA SR-71 longitudinal and lateral-directional dynamics:AIAA-1999-4172[R].Reston:AIAA,1999.
    [3] LEE K H,KIM B S,PARK K E,et al.Estimation of aircraft lateral-directional aerodynamic derivatives from flying quality flight test:AIAA-2001-4014[R].Reston:AIAA,2001.
    [4] ROYSDON P F,KHALID M.Blended-wing-body lateral-directional stability investigation using 6DOF simulation:AIAA-2011-1563[R].Reston:AIAA,2011.
    [5] VECCHIA P D,NICOLOSI F,CILIBERTI D.Aircraft directional stability prediction method by CFD:AIAA-2015-2255[R].Reston:AIAA,2015.
    [6] LEE B,ZAICHIK L,YASHIN Y,et al.Criterion to estimate optimum lateral static stability margin:AIAA-2007-6386[R].Reston:AIAA,2007.
    [7] 乐挺,王立新,况龙.农林飞机近地作业飞行的横航向稳定特性[J].航空学报,2008,29(4):853-858. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB200804015.htm

    YUE T,WANG L X,KUANG L.Lateral stability of an agriculture aircraft during low-altitude flight operation[J].Acta Aeronautica et Astronautica Sinica,2008,29(4):853-858(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB200804015.htm
    [8] 中国民用航空局.运输类飞机适航标准:CCAR-25-R4[S].北京:中国民用航空局,2011:22-23.

    Civil Aviation Administration of China.Airworthiness standards of transport category aircraft:CCAR-25-R4[S].Beijing:Civil Aviation Administration of China,2011:22-23(in Chinese).
    [9] 吴文海.飞行综合控制系统[M].北京:航空工业出版社,2007:157-159.

    WU W H.Integrated flight control system[M].Beijing:Aciation Industry Press,2007:157-159(in Chinese).
    [10] LENOX G W.A flight test determination of the static longitudinal stability of the Cessna 310d airplane[D].Princeton:Princeton University,1961.
    [11] 孙康宁,陆正杰,张景亭.民机横航向静稳定飞行试验与评定方法研究[J].飞行力学,2016,34(1):82-84. http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201601019.htm

    SUN K N,LU Z J,ZHANG J T.Research on the method of flight test and evaluation for lateral and directional stability of civil aircraft[J].Flight Dynamics,2016,34(1):82-84(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201601019.htm
    [12] BURDUN I Y,DALAURENTSI D A,MAVRIS D N.Modeling and simulation of airworthiness requirements for an HSCT prototype in early design:AIAA-1998-4936[R].Reston:AIAA,1998.
    [13] SCHARL J,MAVRIS D N,BURDUN I Y.Use of flight simulation in early design:Formulation and application of the virtual testing and evaluation methodology:AIAA-2000-01-5590[R].Reston:AIAA,2000.
    [14] LIU F,WANG L X,TAN X S.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):112-119. doi: 10.1016/j.cja.2014.12.013
    [15] 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. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201505006.htm

    LIU H L,WANG L X.Assessment of longitudinal ground stability and control for civil aircraft based on digital virtual flight testing method[J].Acta Aeronautica et Astronautica Sinica,2015,36(5):1432-1441(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201505006.htm
    [16] 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. http://bhxb.buaa.edu.cn/CN/abstract/abstract12606.shtml

    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). http://bhxb.buaa.edu.cn/CN/abstract/abstract12606.shtml
    [17] 修忠信,由立岩.运输类飞机合格审定飞行试验指南[M].上海:上海交通大学出版社,2013:92-95,306.

    XIU Z X,YOU L Y.Flight test guide for certification of transport category airplanes[M].Shanghai:Shanghai Jiao Tong University Press,2013:92-95,306(in Chinese).
    [18] Society of Audio Engineering Aerospace.Design objectives for handing qualities of transport aircraft:ARP-4104[R].Warrendale,PA:SAE International,2007.
    [19] 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,2004:2-6.

    GAO H,ZHU P S,GAO Z H.Advanced flight dynamics[M].Beijing:National Defense Industry Press,2004:2-6(in Chinese).
    [20] ABZUG M J.Computational flight dynamics[M].Reston:AIAA,1998:9-17.
    [21] 高金源,李陆豫,冯亚昌.飞机飞行品质[M].北京:国防工业出版社,2003:24-26,139-154.

    GAO J Y,LI L Y,FENG Y C.Aircraft handing qualities[M].Beijing:National Defense Industry Press,2003:24-26,139-154(in Chinese).
    [22] HOSMAN H,STASSEN H.Pilot's perception in the control of aircraft motions[J].Control Engineering Practice,1999,7(11):1421-1429. doi: 10.1016/S0967-0661(99)00111-2
    [23] HOSMAN R,SCHURING J,GEEST P.Pilot model development for the manual balked landing maneuver:AIAA-2005-5884[R].Reston:AIAA,2005.
    [24] POOL D M,MULDER M,ZAAL P M T,et al.Pilot equalization in manual control of aircraft dynamics[C]//Proceedings of the 2009 IEEE International Conference on Systems,Man and Cybernetics.Piscataway,NJ:IEEE Press,2009:2480-2485.
    [25] ZAAL P M T,POLL D M,BRUIN J D,et al.Pilots'use of pitch and heave motion cues in pitch control task:AIAA-2008-6537[R].Reston:AIAA,2008.
    [26] HOSMANG R,VAN D G P,VAN D Z J.Development of a pilot model for the manual balked landing maneuver:AIAA-2009-5818[R].Reston:AIAA,2009.
  • 加载中
图(9) / 表(1)
计量
  • 文章访问数:  795
  • HTML全文浏览量:  91
  • PDF下载量:  528
  • 被引次数: 0
出版历程
  • 收稿日期:  2016-01-29
  • 录用日期:  2016-05-20
  • 网络出版日期:  2017-02-20

目录

    /

    返回文章
    返回
    常见问答