Volume 44 Issue 2
Feb.  2018
Turn off MathJax
Article Contents
CONG Bin, WANG Lixin. Low-order equivalent matching methods for aircraft with flying wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(2): 286-294. doi: 10.13700/j.bh.1001-5965.2017.0044(in Chinese)
Citation: CONG Bin, WANG Lixin. Low-order equivalent matching methods for aircraft with flying wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(2): 286-294. doi: 10.13700/j.bh.1001-5965.2017.0044(in Chinese)

Low-order equivalent matching methods for aircraft with flying wings

doi: 10.13700/j.bh.1001-5965.2017.0044
More Information
  • Corresponding author: WANG Lixin, E-mail:wlx_c818@163.com
  • Received Date: 24 Jan 2017
  • Accepted Date: 24 Apr 2017
  • Publish Date: 20 Feb 2018
  • The low-order equivalent methods are aimed at conventional aircraft. They are not suitable for aircraft with flying wings as a result of flying wings' new handing and stability characteristics. To improve the accuracy and success rate of low-order equivalent matching for aircraft with flying wings, the differences between aircraft with flying wings and conventional aircraft in aerodynamic characteristics, manipulation characteristics, and control system design, are analyzed, and then the research on low-order equivalent methods for aircraft with flying wings is undertaken. The influence of matching frequency range on matching result is obtained via frequency domain characteristic analysis. Square wave signal, 3211 signal, and chirp signal are widely used as input signals for low-order equivalent matching. Their applicability is tested in time domain responses and matching results, and the results show that the square wave signal is most suitable for aircraft with flying wings. The influence of signal strength on matching results is investigated via simulation and analysis. A joint-design method is proposed, in which both directional motions and lateral motions are included in lateral-directional motivating command design. The new method can improve success rate for lateral-directional low-order matching.

     

  • loading
  • [1]
    马松辉, 吴成富, 陈怀民.飞翼飞机稳定性与操纵性研究[J].飞行力学, 2006, 24(3):19-21. http://www.docin.com/p-806432172.html

    MA S H, WU C F, CHEN H M.Study on stability and maneuverability of flying wing aircraft[J].Flight Dynamics, 2006, 24(3):19-21(in Chinese). http://www.docin.com/p-806432172.html
    [2]
    李林, 马超, 王立新.大展弦比飞翼构型的横航向操纵特性[J].北京航空航天大学学报, 2007, 33(10):1186-1190. doi: 10.3969/j.issn.1001-5965.2007.10.014

    LI L, MA C, WANG L X.Lateral-directional control characteristics of high aspect-ratio flying wings configurations[J].Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10):1186-1190(in Chinese). doi: 10.3969/j.issn.1001-5965.2007.10.014
    [3]
    JOHN H.History of low-order equivalent systems for aircraft flying qualities[J].Journal of Guidance, Control, and Dynamics, 2005, 28(4):577-583. doi: 10.2514/1.3787
    [4]
    EUGENE A.Low-order equivalent system identification for the Tu-144LL supersonic transport aircraft[J].Journal of Guidance, Control, and Dynamics, 2003, 26(2):354-362. doi: 10.2514/2.5053
    [5]
    JOHN H, PALOS V. History of low order equivalent systems for aircraft handling qualities analysis and design[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston: AIAA, 2003: 1-13.
    [6]
    谭文倩, 张曙光.飞机横航向等效拟配模型的对比研究[J].飞行力学, 2003, 21(4):14-18. http://www.cnki.com.cn/Article/CJFDTOTAL-FJSJ201001006.htm

    TAN W Q, ZHANG S G.Research on the models of lateral and directional equivalent matching for an aircraft[J].Flight Dynamics, 2003, 21(4):14-18(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-FJSJ201001006.htm
    [7]
    崔益华, 韩意新, 陈永亮.电传飞机低阶等效系统频域辨识新方法[J].南京航空航天大学学报, 2016, 48(3):432-437. http://www.cqvip.com/QK/92509X/201603/669359080.html

    CUI Y H, HAN Y X, CHEN Y L.New frequency domain identification method for FBW aircraft based on low order equivalent system[J].Journal of Nanjing University of Aeronautics and Astronautics, 2016, 48(3):432-437(in Chinese). http://www.cqvip.com/QK/92509X/201603/669359080.html
    [8]
    冀翔, 夏洁.基于短时傅里叶变换的飞控纵向频域等效拟配[J].北京航空航天大学学报, 2011, 37(7):872-876. http://bhxb.buaa.edu.cn/CN/abstract/abstract12025.shtml

    JI X, XIA J.Longitudinal frequency-domain equivalent matching method for flight control system based on short time Fourier transform[J].Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(7):872-876(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract12025.shtml
    [9]
    张勇.低阶等效系统方法的发展历史[J].飞行力学, 2011, 29(6):1-3. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=fxlx201106001

    ZHANG Y.Development history of low order equivalent systems for aircraft handling qualities analysis and design[J].Flight Dynamics, 2011, 29(6):1-3(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=fxlx201106001
    [10]
    何明胜. 飞行品质分析中的低阶等效模型研究[D]. 西安: 西安电子科技大学, 2006: 1-8.

    HE M S. Research on low-order equivalent model in aircraft handling qualities[D]. Xi'an: Xidian University, 2006: 1-8(in Chinese).
    [11]
    田海燕. 飞行品质中低阶等效系统的研究[D]. 西安: 西安电子科技大学, 2008: 1-12.

    TIAN H Y. Research on low-order equivalent system in aircraft handling qualities[D]. Xi'an: Xidian University, 2008: 1-12(in Chinese).
    [12]
    李淼, 王立新, 李林.小展弦比飞翼构型作战飞机短周期品质评定方法[J].飞行力学, 2009, 27(5):21-27. http://d.wanfangdata.com.cn/Periodical_fxlx200905006.aspx

    LI M, WANG L X, LI L.Qualities assesses criterion of short period mode for flying wings with low aspect-ratio[J].Flight Dynamics, 2009, 27(5):21-27(in Chinese). http://d.wanfangdata.com.cn/Periodical_fxlx200905006.aspx
    [13]
    李林, 王立新.大展弦比飞翼作战飞机横航向飞行品质特性[J].北京航空航天大学学报, 2009, 35(6):661-664. http://bhxb.buaa.edu.cn/CN/abstract/abstract8804.shtml

    LI L, WANG L X.Lateral-directional flying quality characteristics of high aspect-ratio combat flying wings[J].Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(6):661-664(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract8804.shtml
    [14]
    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, 2003:261-264.

    GAO J Y, LI L Y, FENG Y C, et al.Aircraft flying qualities[M].Beijing:National Defense Industry Press, 2003:261-264(in Chinese).
    [15]
    Department of Defence. Flying qualities of piloted aircraft: MIL-STD-1797[S]. Washington, D. C. : Department of Defence, 1990.
    [16]
    王磊, 王立新, 贾重任.飞翼布局飞机开裂式方向舵作用特性和使用特点[J].航空学报, 2011, 32(8):1392-1399. http://d.g.wanfangdata.com.cn/Periodical_hkxb201108002.aspx

    WANG L, WANG L X, JIA Z R.Control features and application characteristics of split drag rudder utilized by flying wing[J].Acta Aeronautica et Astronautica Sinica, 2011, 32(8):1392-1399(in Chinese). http://d.g.wanfangdata.com.cn/Periodical_hkxb201108002.aspx
    [17]
    MA C, WANG L X. Flying-wing aircraft control allocation[C]//47th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2009.
  • 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

    Figures(10)  / Tables(6)

    Article Metrics

    Article views(826) PDF downloads(607) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return