Differential Structure of Inductive Proximity Sensor

The inductive proximity sensor (IPS) is applicable to displacement measurements in the aviation field due to its non-mechanical contact, safety, and durability. IPS can increase reliability of position detection and decrease maintenance cost of the system effectively in aircraft applications. Nevert...

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Main Authors: Yi-Xin Guo, Cong Lai, Zhi-Biao Shao, Kai-Liang Xu, Ting Li
Format: Article
Language:English
Published: MDPI AG 2019-05-01
Series:Sensors
Subjects:
Online Access:https://www.mdpi.com/1424-8220/19/9/2210
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spelling doaj-cd3638cd43b14a6b8687e45d364178012020-11-25T00:15:25ZengMDPI AGSensors1424-82202019-05-01199221010.3390/s19092210s19092210Differential Structure of Inductive Proximity SensorYi-Xin Guo0Cong Lai1Zhi-Biao Shao2Kai-Liang Xu3Ting Li4School of Electronic and Information Engineering, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shaanxi 710049, ChinaSchool of Electronic and Information Engineering, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shaanxi 710049, ChinaSchool of Electronic and Information Engineering, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shaanxi 710049, ChinaSchool of Automation and Information Engineering, Xi’an University of Technology, No. 5 South Jinhua Road, Xi’an, Shaanxi 710048, ChinaSchool of Electronic and Information Engineering, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shaanxi 710049, ChinaThe inductive proximity sensor (IPS) is applicable to displacement measurements in the aviation field due to its non-mechanical contact, safety, and durability. IPS can increase reliability of position detection and decrease maintenance cost of the system effectively in aircraft applications. Nevertheless, the specialty in the aviation field proposes many restrictions and requirements on the application of IPS, including the temperature drift effect of the resistance component of the IPS sensing coil. Moreover, reliability requirements of aircrafts restrict the use of computational-intensive algorithms and avoid the use of process control components. Furthermore, the environment of airborne electronic equipment restricts measurements driven by large current and proposes strict requirements on emission tests of radio frequency (RF) energy. For these reasons, a differential structured IPS measurement method is proposed in this paper. This measurement method inherits the numerical separation of the resistance and inductance components of the IPS sensing coil to improve the temperature adaptation of the IPS. The computational complexity is decreased by combining the dimension-reduced look-up table method to prevent the use of process control components. The proposed differential structured IPS is equipped with a differential structure of distant and nearby sensing coils to increase the detection accuracy. The small electric current pulse excitation decreases the RF energy emission. Verification results demonstrate that the differential structured IPS realizes the numerical decoupling calculation of the vector impedance of the sensing coil by using 61 look-up table units. The measuring sensitivity increased from 135.5 least significant bits (LSB)/0.10 mm of a single-sensing-coil structured IPS to 1201.4 LSB/0.10 mm, and the linear approximation distance error decreased from 99.376 μm to −3.240 μm. The proposed differential structured IPS method has evident comparative advantages compared with similar measuring techniques.https://www.mdpi.com/1424-8220/19/9/2210inductive proximity sensordisplacement measurementsdifferential structurelinear approximation methodlook-up tableairborne electronic equipmentsmall electric current pulse
collection DOAJ
language English
format Article
sources DOAJ
author Yi-Xin Guo
Cong Lai
Zhi-Biao Shao
Kai-Liang Xu
Ting Li
spellingShingle Yi-Xin Guo
Cong Lai
Zhi-Biao Shao
Kai-Liang Xu
Ting Li
Differential Structure of Inductive Proximity Sensor
Sensors
inductive proximity sensor
displacement measurements
differential structure
linear approximation method
look-up table
airborne electronic equipment
small electric current pulse
author_facet Yi-Xin Guo
Cong Lai
Zhi-Biao Shao
Kai-Liang Xu
Ting Li
author_sort Yi-Xin Guo
title Differential Structure of Inductive Proximity Sensor
title_short Differential Structure of Inductive Proximity Sensor
title_full Differential Structure of Inductive Proximity Sensor
title_fullStr Differential Structure of Inductive Proximity Sensor
title_full_unstemmed Differential Structure of Inductive Proximity Sensor
title_sort differential structure of inductive proximity sensor
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2019-05-01
description The inductive proximity sensor (IPS) is applicable to displacement measurements in the aviation field due to its non-mechanical contact, safety, and durability. IPS can increase reliability of position detection and decrease maintenance cost of the system effectively in aircraft applications. Nevertheless, the specialty in the aviation field proposes many restrictions and requirements on the application of IPS, including the temperature drift effect of the resistance component of the IPS sensing coil. Moreover, reliability requirements of aircrafts restrict the use of computational-intensive algorithms and avoid the use of process control components. Furthermore, the environment of airborne electronic equipment restricts measurements driven by large current and proposes strict requirements on emission tests of radio frequency (RF) energy. For these reasons, a differential structured IPS measurement method is proposed in this paper. This measurement method inherits the numerical separation of the resistance and inductance components of the IPS sensing coil to improve the temperature adaptation of the IPS. The computational complexity is decreased by combining the dimension-reduced look-up table method to prevent the use of process control components. The proposed differential structured IPS is equipped with a differential structure of distant and nearby sensing coils to increase the detection accuracy. The small electric current pulse excitation decreases the RF energy emission. Verification results demonstrate that the differential structured IPS realizes the numerical decoupling calculation of the vector impedance of the sensing coil by using 61 look-up table units. The measuring sensitivity increased from 135.5 least significant bits (LSB)/0.10 mm of a single-sensing-coil structured IPS to 1201.4 LSB/0.10 mm, and the linear approximation distance error decreased from 99.376 μm to −3.240 μm. The proposed differential structured IPS method has evident comparative advantages compared with similar measuring techniques.
topic inductive proximity sensor
displacement measurements
differential structure
linear approximation method
look-up table
airborne electronic equipment
small electric current pulse
url https://www.mdpi.com/1424-8220/19/9/2210
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AT zhibiaoshao differentialstructureofinductiveproximitysensor
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AT tingli differentialstructureofinductiveproximitysensor
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