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Resonance Effect Decrease and Accuracy Increase of Piezoelectric Accelerometer Measurement by Appropriate Choice of Frequency Range
- Source :
- Shock and Vibration, Vol 2018 (2018)
- Publication Year :
- 2018
- Publisher :
- Hindawi Limited, 2018.
-
Abstract
- A suitable piezoelectric accelerometer mathematical model is proposed to extract a relationship of motion relative frequency as a function of natural frequency. This relationship helps to select appropriate accelerometer frequency range that minimizes measurement error and improves accuracy. It also allows deducing a formula relating the damping rate and the measurement error of the accelerometer. To protect the accelerometer from failure, the resonance phenomenon effect must be minimized. In order to achieve this objective, physical principle is modeled to find a precise relationship which can determine the accelerometer appropriate frequency range. The developed model was simulated and the obtained results have showed that the selection of the frequency range has minimized the measurement error, increased the accelerometer accuracy, and reduced the resonance effect. Finally a comparative study was conducted to show the importance of the obtained results compared to recent literatures.
- Subjects :
- 0209 industrial biotechnology
Article Subject
Computer science
Acoustics
02 engineering and technology
Accelerometer
01 natural sciences
020901 industrial engineering & automation
Range (statistics)
Resonance effect
Civil and Structural Engineering
Observational error
Piezoelectric accelerometer
Mechanical Engineering
010401 analytical chemistry
Resonance
Natural frequency
Function (mathematics)
Geotechnical Engineering and Engineering Geology
Condensed Matter Physics
lcsh:QC1-999
0104 chemical sciences
Computer Science::Other
Mechanics of Materials
ComputerSystemsOrganization_MISCELLANEOUS
lcsh:Physics
Subjects
Details
- Language :
- English
- ISSN :
- 18759203 and 10709622
- Volume :
- 2018
- Database :
- OpenAIRE
- Journal :
- Shock and Vibration
- Accession number :
- edsair.doi.dedup.....b55f0a6647f56d95856efe5f8153fa14