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    • 2. 发明申请
    • Measurement method for aviation-specific proximity sensor
    • 航空专用接近传感器的测量方法
    • US20150051857A1
    • 2015-02-19
    • US14386817
    • 2012-03-22
    • Zhibiao ShaoYixin Guo
    • Zhibiao ShaoYixin Guo
    • G01B7/00G01R27/26
    • G01B7/003G01D5/243G01R27/2611
    • A measurement method for an aviation-specific inductive proximity sensor (IPS for short) includes steps of: 1) building a measurement circuit, wherein an IPS comprises an internal resistance r and an inductance L; 2) building a look-up table, wherein the step 2) specifically comprises steps of: sampling a first voltage measured value U1 corresponding to a first constant delay time T1 with the ADC; sampling a second voltage measured value U2 corresponding to a second constant delay time T2 with the ADC; then obtaining voltage discharge formulas U1(T1, R, r, L) and U2(T2, R, r, L) of an r-L circuit; and 3) compressing the look-up table, utilizing the compressed look-up table for calculation during measurement. The present invention ensures that the system works within a standard temperature range, and improves measurement stability, reliability, and real-time performance. Furthermore, there is no floating point calculation, which saves CPU or MCU hardware resources.
    • 一种用于航空专用电感式接近传感器(IPS)的测量方法包括以下步骤:1)构建测量电路,其中IPS包括内部电阻r和电感L; 2)构建查找表,其中步骤2)具体包括以下步骤:对与ADC对应的第一恒定延迟时间T1的第一电压测量值U1进行采样; 用ADC对与第二恒定延迟时间T2对应的第二电压测量值U2进行采样; 然后获得r-L电路的电压放电公式U1(T1,R,r,L)和U2(T2,R,r,L); 3)压缩查表,利用压缩查表来计算测量。 本发明确保系统在标准温度范围内工作,并提高测量稳定性,可靠性和实时性能。 此外,没有浮点计算,可节省CPU或MCU硬件资源。