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连续变迎角试验数据自适应分段拟合滤波方法

王南天 王雄 孙鹏 许晓斌 邹琼芬

王南天, 王雄, 孙鹏, 等 . 连续变迎角试验数据自适应分段拟合滤波方法[J]. 北京航空航天大学学报, 2021, 47(6): 1145-1151. doi: 10.13700/j.bh.1001-5965.2020.0145
引用本文: 王南天, 王雄, 孙鹏, 等 . 连续变迎角试验数据自适应分段拟合滤波方法[J]. 北京航空航天大学学报, 2021, 47(6): 1145-1151. doi: 10.13700/j.bh.1001-5965.2020.0145
WANG Nantian, WANG Xiong, SUN Peng, et al. Self-adaptive piecewise fitting filtering method for test data in continuous sweeping angle of attack[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(6): 1145-1151. doi: 10.13700/j.bh.1001-5965.2020.0145(in Chinese)
Citation: WANG Nantian, WANG Xiong, SUN Peng, et al. Self-adaptive piecewise fitting filtering method for test data in continuous sweeping angle of attack[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(6): 1145-1151. doi: 10.13700/j.bh.1001-5965.2020.0145(in Chinese)

连续变迎角试验数据自适应分段拟合滤波方法

doi: 10.13700/j.bh.1001-5965.2020.0145
详细信息
    通讯作者:

    王南天. E-mail: wangnant@126.com

  • 中图分类号: V216.1

Self-adaptive piecewise fitting filtering method for test data in continuous sweeping angle of attack

More Information
  • 摘要:

    针对常用的阶梯变迎角数据处理方法处理连续变迎角试验数据时,不能去除低频振动分量的问题,基于试验数据中的近似对称、局部线性等特点,提出一种将数据进行分段二项式拟合的处理方法,并详细论述其基本原理,重点介绍基于方差极小值动态确定数据分段长度的方法。基于测试信号的实验结果表明所提方法可将低频分量信号滤除近70%,有效提高数据处理精度。经标模试验测试验证,所提方法可成功应用于某些试验。

     

  • 图 1  连续变迎角试验数据及其功率谱

    Figure 1.  Data of continuous sweeping angle of attack test and its power spectrum

    图 2  振动数据误差特性

    Figure 2.  Error characteristics of vibration data

    图 3  方法实现步骤

    Figure 3.  Implementation steps of proposed method

    图 4  某试验数据及拟合方差

    Figure 4.  Data of a test and its fitting variance

    图 5  数据分段

    Figure 5.  Data segmentation

    图 6  长度搜索过程中的方差变化

    Figure 6.  Variance change during length search

    图 7  分段拟合结果

    Figure 7.  Results of piecewise fitting

    图 8  滤波结果及对应残差

    Figure 8.  Filtered results and corresponding residuals

    图 9  测试信号

    Figure 9.  Test signal

    图 10  测试信号滤波结果及对应残差

    Figure 10.  Filtered results and corresponding residuals of test signal

    图 11  测试信号及滤波后的功率谱

    Figure 11.  Power spectrum of test signals and filtered results

    图 12  某高超标模测试结果

    Figure 12.  Test results of a hypervelocity normal mode

    图 13  某试验模型测试结果

    Figure 13.  Test results based on some test model

    表  1  试验数据分析结果

    Table  1.   Analyzed results of test data

    y powerk/% power_pk/% max_dertak/% max_derta_pk/% dertak/10-6 derta_pk/10-6
    y1 0.104 4 0.115 2 0.222 3 0.245 9 -10.07 -11.11
    y2 0.035 7 0.039 4 0.083 3 0.092 0 7.91 8.73
    34.24 34.24 37.40 37.40 -78.52 -78.52
    下载: 导出CSV

    表  2  滤波效果分析

    Table  2.   Analyzed filtering results

    α/(°) 阶梯数据U0/V 滤波前数据U1/V 滤波后数据U2/V 滤波前偏差e1/% 滤波后偏差e2/%
    -6.45 0.959 8 0.955 8 0.955 2 -0.41 -0.47
    -4.30 0.911 6 0.912 4 0.908 7 0.09 -0.32
    -3.24 0.878 7 0.880 4 0.881 1 0.19 0.28
    -2.20 0.832 8 0.829 9 0.833 8 -0.35 0.12
    -1.79 0.803 1 0.807 2 0.805 8 0.52 0.33
    -1.16 0.762 7 0.767 1 0.769 2 0.58 0.85
    -0.13 0.734 0 0.735 9 0.735 3 0.27 0.19
    0.28 0.758 8 0.756 9 0.761 3 -0.25 0.33
    0.91 0.805 4 0.809 5 0.804 7 0.52 -0.08
    1.97 0.805 2 0.812 6 0.812 1 0.93 0.86
    3.02 0.809 4 0.809 3 0.812 8 -0.01 0.41
    4.08 0.851 6 0.851 9 0.851 6 0.04 0
    6.20 0.904 2 0.902 9 0.902 8 -0.13 -0.14
    下载: 导出CSV
  • [1] 舒海峰, 许晓斌, 孙鹏. 高超声速风洞多天平测力试验技术研究[J]. 实验流体力学, 2014, 28(4): 49-53. https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC201404008.htm

    SHU H F, XU X B, SUN P. Technology investigation on force test with multi-balance in hypersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(4): 49-53(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC201404008.htm
    [2] 谢艳, 李平, 王瑞波, 等. 2.4米跨声速风洞连续变攻角测力试验技术研究[J]. 气动研究与发展, 2009, 19(3): 10-14.

    XIE Y, LI P, WANG R B, et al. An experimental investigation on force measurement of continuous angle of attack traverses in 2.4 m transonic wind tunnel[J]. Aerodynamics Research and Development, 2009, 19(3): 10-14(in Chinese).
    [3] 魏志, 谢艳, 吴军强, 等. 连续变攻角测力试验技术在大型暂冲式跨声速风洞中的应用[J]. 实验流体力学, 2011, 25(4): 99-102. doi: 10.3969/j.issn.1672-9897.2011.04.019

    WEI Z, XIE Y, WU J Q, et al, Application of continuous sweeping force measuring technology in large intermittent transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(4): 99-102(in Chinese). doi: 10.3969/j.issn.1672-9897.2011.04.019
    [4] 黄辉, 黄昊宇, 凌忠伟, 等. Φ0.5米高超声速风洞连续变攻角测力试验数据处理方法研究[J]. 计算机测量与控制, 2019, 27(8): 281-285. https://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201908060.htm

    HUANG H, HUANG H Y, LING Z W, et al. Research on data processing method of continuous variable angle of attack force in Φ0.5 m hypersonic wind tunne[J]. Computer Measurement & Control, 2019, 27(8): 281-285(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JZCK201908060.htm
    [5] 唐志共, 许晓斌, 杨彦广, 等. 高超声速风洞气动力试验技术进展[J]. 航空学报, 2015, 36(1): 86-97. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201501007.htm

    TANG Z G, XU X B, YANG Y G, et al. Research progress on hypersonic wind tunnel aerodynamic testing techniques[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 86-97(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201501007.htm
    [6] 张俊. 工程实用的飞行器低速风洞连续扫描试验技术研究[D]. 长沙: 国防科学技术大学, 2007.

    ZHANG J. Investigation of the continuous scan technology on engineer to aircraft in low speed wind tunnel[D]. Changsha: National University of Defense Technology, 2007(in Chinese).
    [7] 唐乔乔, 张卫国, 刘忠华, 等. 8 m×6 m风洞特大迎角机构连续扫描试验技术研究与应用[J]. 实验流体力学, 2012, 26(2): 81-85. doi: 10.3969/j.issn.1672-9897.2012.02.018

    TANG Q Q, ZHANG W G, LIU Z H, et al. Research and application of the continuous scan technique to the high angle of attack equipment in 8 m×6 m wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(2): 81-85(in Chinese). doi: 10.3969/j.issn.1672-9897.2012.02.018
    [8] 张双喜, 盖文, 褚卫华, 等. 风洞试验连续变攻角控制策略[J]. 计算机测量与控制, 2014, 22(2): 390-396. doi: 10.3969/j.issn.1671-4598.2014.02.025

    ZHANG S X, GAI W, CHU W H, et al. Control strategy of uniform changing attack angle in wind tunnel[J]. Computer Measurement & Control, 2014, 22(2): 390-396(in Chinese). doi: 10.3969/j.issn.1671-4598.2014.02.025
    [9] 孟宝清, 韩桂来, 姜宗林. 结构振动对大型激波风洞气动力测量的干扰[J]. 力学学报, 2016, 48(1): 102-110. https://www.cnki.com.cn/Article/CJFDTOTAL-LXXB201601012.htm

    MENG B Q, HAN G L, JIANG Z L. Theoretical investigation on aerodynamic force measurement interfered by structural vibrations in large shock tunnel[J]. Chinese Journal of Theoretical and Applied Mechanics, 2016, 48(1): 102-110(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-LXXB201601012.htm
    [10] 程忠宇, 陈宏, 张琦. 多加速度计振动分离惯性补偿测力技术[J]. 流体力学实验与测量, 1993, 13(4): 57-61. https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199904012.htm

    CHENG Z Y, CHEN H, ZHANG Q. Inertia compensation technology based on multi-accelerometer vibration separating[J]. Experiments and Measurements in Fluid Mechanics, 1993, 13(4): 57-61(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199904012.htm
    [11] 吕金州, 张小庆, 陈光雄, 等. 基于惯性补偿的脉冲风洞测力天平瞬态研究[J]. 振动与冲击, 2018, 37(2): 216-222. https://www.cnki.com.cn/Article/CJFDTOTAL-ZDCJ201802032.htm

    LV J Z, ZHANG X Q, CHEN G X, et al. Transient simulation for dynamic output of force measuring balance in animpulse combustion wind tunnel based on intertia compensation[J]. Journal of Vibration and Shock, 2018, 37(2): 216-222(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-ZDCJ201802032.htm
    [12] 艾迪, 许晓斌, 王雄. 风洞天平动态特性多阶惯性补偿技术研究[J]. 实验流体力学, 2018, 32(4): 87-92. https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC201804011.htm

    AI D, XU X B, WANG X. Investigation of wind tunnel balance dynamic characteristics' multi-order inertial compensation[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(4): 87-92(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-LTLC201804011.htm
    [13] 张鹏, 谢艳, 孙宁, 等. 基于改进小波阈值函数的风洞连续信号降噪方法[J]. 计算机测量与控制, 2014, 22(4): 1300-1302. doi: 10.3969/j.issn.1671-4598.2014.04.103

    ZHANG P, XIE Y, SUN N, et al. Wind tunnel continuous signal de-noising method based on improved thresholding function[J]. Computer Measurement & Control, 2014, 22(4): 1300-1302(in Chinese). doi: 10.3969/j.issn.1671-4598.2014.04.103
    [14] 张鹏, 刘晨雨, 曹宇晴. 基于Matlab GUI的风洞信号小波分析处理软件[J]. 兵工自动化, 2018, 37(1): 61-67. https://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201801016.htm

    ZHANG P, LIU C Y, CAO Y Q. Analysis and processing software of wind tunnel signals on the basis of the Matlab GUI programming[J]. Ordnance Industry Automation, 2018, 37(1): 61-67(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201801016.htm
    [15] 张鹏, 魏志, 王春, 等. 基于小波变换的风洞连续信号降噪分析[J]. 兵工自动化, 2013, 32(5): 63-67. https://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201305016.htm

    ZHANG P, WEI Z, WANG C, et al. Analysis of wind tunnel continuous signal de-noising based on wavelet transformation[J]. Ordnance Industry Automation, 2013, 32(5): 63-67(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201305016.htm
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出版历程
  • 收稿日期:  2020-04-16
  • 录用日期:  2020-07-10
  • 网络出版日期:  2021-06-20

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