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 |