Volume 13 Issue 2
. 
Turn off MathJax
Article Contents
Article Navigation >  Journal of Traffic and Transportation Engineering  > 2013  >  13(2): 66-72
Next Previous
CAI Liang-cai, WANG Hai-fu, ZHU Zhan-qing, ZHONG Xiao-lei. Calculation method of running distance for aircraft takeoff on plateau airport[J]. Journal of Traffic and Transportation Engineering, 2013, 13(2): 66-72. doi: 10.19818/j.cnki.1671-1637.2013.02.010
Citation: CAI Liang-cai, WANG Hai-fu, ZHU Zhan-qing, ZHONG Xiao-lei. Calculation method of running distance for aircraft takeoff on plateau airport[J]. Journal of Traffic and Transportation Engineering, 2013, 13(2): 66-72. doi: 10.19818/j.cnki.1671-1637.2013.02.010
shu

Calculation method of running distance for aircraft takeoff on plateau airport

doi: 10.19818/j.cnki.1671-1637.2013.02.010

  • Department of Airport and Architecture Engineering, Air Force Engineering University, Xi'an 710038, Shaanxi, China

More Information
  • Author Bio:

    CAI Liang-cai(1960-), male, professor, PhD, +86-29-84787008, liangcai07@126.com

  • Received Date: 2012-09-18
  • Publish Date: 2013-04-25
    Abstract
  • Aiming at the complicated environment of plateau airport and the characteristic of significant decline for aircraft engine performance, the running process of aircraft takeoff on plateau airport was analyzed. The practical pressure of airport was transformed into standard atmosphere pressure, the running distances under different times were calculated by using the correctional instantaneous thrust of aircraft engine, and the calculation method of running distance for aircraft takeoff on plateau airport was put out. The influences of altitude, takeoff mass, temperature and wind speed on the running distances of aircraft takeoff were analyzed, the simplification formula of running distance was put forward, and example verification was carried out. Analysis result shows that when altitude is 3 569.5 m, temperature is 16.4 ℃ and upwind speed is 2.1 m·s-1, the maximum absolute error between the running distance calculated by the proposed method and test running distance for aircraft Ⅰ is no more than 48 m, and the maximum relative error is no more than 2.7%. The maximum absolute error between the running distance calculated by the proposed method and test running distance for aircraft Ⅱ is no more than 100 m, and the maximum relative error is no more than 4.2%, The maximum relative errors between the running distances calculated by simplification formula and test running distances for aircraft Ⅰ and aircraft Ⅱ are 3.9% and 2.8% respectively, which meet the engineering requirement.

     

    • FullText(HTML)
  • loading
    • References(23)
  • [1]
    WANG Zhen-hui, CAI Liang-cai, SHAO Bin. Design method of military airfield runway length[J]. Journal of Transportation Engineering and Information, 2007, 5(1): 67-70, 76. (in Chinese). doi: 10.3969/j.issn.1672-4747.2007.01.013
    [2]
    CAI Liang-cai, ZHENG Ru-hai, CHONG Xiao-lei, et al. Test and analyses of airplane's running distance of taking-off and landing on plateau airport[J]. Journal of Air Force Engineering University: Natural Science Edition, 2000, 1(2): 4-7. (in Chinese). doi: 10.3969/j.issn.1009-3516.2000.02.002
    [3]
    SONG Hua-yu, CAI Liang-cai, WU Li-rong, et al. Calculation of aircraft taking-off running distance based on BP network[J]. Journal of Air Force Engineering University: Natural Science Edition, 2004, 5(6): 4-6. (in Chinese). doi: 10.3969/j.issn.1009-3516.2004.06.002
    [4]
    YANG Hong-ping, WANG Li-xin, LI Qin-hong. An engineering method to determine the minimum unstick speed of civil airplanes[J]. Flight Dynamics, 2006, 24(2): 9-12. (in Chinese). doi: 10.3969/j.issn.1002-0853.2006.02.003
    [5]
    DENG Yang-chen, ZHANG Shuang, CHEN Hua, et al. The optimal taxi-distance determining on aircraft take-off and landing[J]. Aeronautical Computing Technique, 2006, 36(1): 71-74, 78. (in Chinese). doi: 10.3969/j.issn.1671-654X.2006.01.021
    [6]
    ZHANG Zhi-gang, WANG Bai-zheng, WANG He-ping, et al. Research on take-off performance of the MA60aircraft at plateau airport[J]. Flight Dynamics, 2006, 24(4): 65-69. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX200604016.htm
    [7]
    AC 150/5300-13B, airport design[S].
    [8]
    GE Zhi-hao, XU Hao-jun, MENG Jie. Research on pilot model random and numerical simulation[J]. Journal of System Simulation, 2007, 19(2): 453-455. (in Chinese). doi: 10.3969/j.issn.1004-731X.2007.02.057
    [9]
    LI Qiu-hong, SUN Jian-guo, WANG Qian-yu. A new method for estimating the thrust of aircraft engines[J]. Control Theory and Applications, 2011, 28(2): 185-191. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-KZLY201102010.htm
    [10]
    PINDER S D. Aircraft takeoff performance monitoring in farnorthern regions: an application of the global positioning system[D]. Saskatoon: University of Saskatchewan, 2003.
    [11]
    BALL T, TUMER S, MARSHALL D D. Short takeoff per-formance using circulation control[C]//AIAA. 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2008: 1-14.
    [12]
    ZHAO Yong-ping, SUN Jian-guo. Aeroengine thrust estimation using least squares support vector regression machine[J]. Journal of Aerospace Power, 2009, 24(6): 1420-1425. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI200906036.htm
    [13]
    SONG Hua-yu. A numerical value confirmation method of engine thrustin aircraft in take-off running[J]. Aeronautical Computing Technique, 2010, 40(6): 43-46. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKJJ201006012.htm
    [14]
    XUE Hong-tao, WANG Ke-bo. Military aircraft takeoff and landing planning and computing based on performance model[J]. Computer Engineering and Design, 2011, 32(5): 1837-1840. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-SJSJ201105080.htm
    [15]
    WANG Hui, ZHANG Wei-fang. Construction of a real-time flight simulation system based on computer environment[J]. Mechanical Science and Technology for Aerospace Engineering, 2011, 30(8): 1235-1238. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JXKX201108005.htm
    [16]
    WU Li-rong. Basic research on performance desgin and use technology for modern aircraft and engine on plateau region[D]. Xi'an: Air Force Engineering University, 2004. (in Chinese).
    [17]
    YU Xiao-jing, HE Guo-qiang, LI Jiang, et al. Calculating effects of relevant parameters on vortex valve control of variable thrust SMR[J]. Journal of Northwestern Polytechnical University, 2009, 27(2): 178-183. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-XBGD200902009.htm
    [18]
    CAI Liang-cai, WANG Sheng, ZHENG Ru-hai, et al. Test and analysis of airplane's running track in taking off and landing[J]. Journal of Southeast University: Natural Science Edition, 2002, 32(2): 264-267. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-DNDX200202025.htm
    [19]
    WANG He-wei. The study on calculation method of runway length on plateau military airport[D]. Xi'an: Air Force Engineering University, 2000. (in Chinese).
    [20]
    GE Zhi-hao, XU Hao-jun, HU Fei, et al. MATLAB simulation model of closed-loop aircraft-pilot system[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2004, 24(3): 389-391. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-DJZD2004S6043.htm
    [21]
    WANG Chun-guang, LI Gui-xian, ZHENG Shu-tao, et al. Characteristic analysis of optimal control behavior of pilot sliding[J]. Journal of Harbin Institute of Technology, 2011, 43(3): 38-43. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HEBX201103009.htm
    [22]
    GAO Jian, ZHENG Shu-tao, HAN Jun-wei. Pilot model parameters identification based least square method[J]. Journal of Jiangnan University: Natural Science Edition, 2011, 10(6): 648-652. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JLXY201106005.htm
    [23]
    LI Da-wei, XU Hao-jun, HU Xin-jiang, et al. Research on stability of aircraft-pilot closed loop system based on matching of equivalent system[J]. Flight Dynamics, 2011, 29(4): 19-22. (in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FHLX201104005.htm
    • Relative Articles
    • Supplements(0)
    • Cited By

Catalog

    Get Citation
    PDF
    XML

    Article Metrics

    Article views (2379) PDF downloads(3111) Cited by()
    Related

    Website copyright Journal of Traffic and Transportation Engineering Editorial Department陕ICP备05001904号-1

    Address ：Editorial Department of Journal of Traffic and Transportation Engineering, Chang'an University, Middle Section of South 2nd Ring Road, Xi'an, China（710064） Tel：029-82334388 Email：jygc@gfscw.cn

    All visit:Today's visit:

    Supported by: Beijing Renhe Information Technology Co. Ltd    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return