A Self-Temperature Compensation Barometer Based on All-Quartz Resonant Pressure Sensor

  • 0Research Center of Structural Health Monitoring and Prognosis, State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.

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Summary

This summary is machine-generated.

This study presents a self-temperature compensating barometer using a novel quartz resonant sensor. It achieves high accuracy (0.019% F.S.) across wide temperature and pressure ranges, verified by drone flight tests.

Area Of Science

  • Physics
  • Materials Science
  • Sensor Technology

Background

  • Quartz resonant pressure sensors offer high sensitivity but are susceptible to temperature variations.
  • Accurate barometric pressure readings are crucial for various applications, including meteorology and navigation.

Purpose Of The Study

  • To develop a self-temperature compensating barometer.
  • To improve the accuracy and stability of quartz resonant pressure sensors under varying temperatures.

Main Methods

  • Designed and fabricated a novel sensor chip with a double-ended tuning fork (DETF) resonator for pressure sensing and a single-ended tuning fork (SETF) resonator for temperature compensation.
  • Implemented a polynomial fitting method for temperature compensation.
  • Conducted experimental tests across a pressure range of 200-1200 hPa and a temperature range of -20°C to +60°C.

Main Results

  • Achieved an accuracy of 0.019% F.S. within the tested ranges.
  • Demonstrated absolute errors within ±23 Pa.
  • Verified performance through a drone flight test, showing consistency with actual flight trajectory.

Conclusions

  • The novel quartz resonant pressure sensor effectively compensates for temperature drift.
  • The developed barometer exhibits high accuracy and stability for practical applications.
  • Drone flight tests confirm the sensor's real-world performance and reliability.

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