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Development of MEMS Pressure Sensor-based Pressure Calibrator

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dc.contributor.author Project Supervisor: Dr. Amir Hamza Dr. Mubashir Saleem Dr. Hamid Jabbar Mr. Usman Sani (NESCOM), Arslan Falak Muhammad Haseeb Tariq GC Chaudhary Ali Usman
dc.date.accessioned 2025-03-04T10:37:47Z
dc.date.available 2025-03-04T10:37:47Z
dc.date.issued 2022
dc.identifier.other DE-MTS-40
dc.identifier.uri http://10.250.8.41:8080/xmlui/handle/123456789/50501
dc.description Project Supervisor: Dr. Amir Hamza Dr. Mubashir Saleem Dr. Hamid Jabbar Mr. Usman Sani (NESCOM) en_US
dc.description.abstract Pressure calibrators are imported at huge costs but if manufactured locally, the costs could be reduced to an affordable margin. With this motivation, a MEMS pressure sensor-based Pressure Calibration simulator was designed and manufactured. A Baro-altimeter measures the height of an aircraft by calculation of air pressure at that location. The pressure inside the Baro-altimeter is decreased artificially to a point where the aircraft is up in the air and the pressure sensors of the aircraft are calibrated and checked for faults. The mechanism creates a vacuum inside the tubes and the pressure is read by a highly accurate MEMS pressure sensor that is used as a reference and a device under test that is a low-quality pressure sensor. The data is fed into a microcontroller STM32 through ADS1248 and after comparing readings from both sensors, the results are displayed. en_US
dc.language.iso en en_US
dc.publisher College of Electrical & Mechanical Engineering (CEME), NUST en_US
dc.title Development of MEMS Pressure Sensor-based Pressure Calibrator en_US
dc.type Project Report en_US


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