• HARSHA K
• KEHKESHAN JALALL S
• RASHMI RANI SAMANTRAY
• KHAMER FATHIMA U BOODIHAL

The main idea behind this project is to provide the real-time alerts to the pilot on flight regarding the fuel quantity, tank status and the sensor failure. In the ancient time, the system used was not much updated. It did not have provision for the switching, error message display on LCD and if the system is unstable there might be tilt in the system. The olden days system used to vary the fuel calibration with the variation in the system, but in the current system even if the system is unstable the fuel will be displayed with precision. When the main tank used to be empty the was no feature of taking the fuel from auxiliary tanks automatically. In the present system proposed in this report when the fuel in the main tank reaches a minimal level then the fuel will be automatically transferred to the main tank from the auxiliary tank 1 and 2 respectively. When there arises a problem in the module it’s difficult to find error in a particular tank or sensor, but this problem can be easily determined in the current scenario of the module because it will display an error message for a particular tank or sensor. Thus error detection becomes easier.

Fuel display, LCD, ARM7LPC2148, caliberation

"Calibration and Volumetric Measurement of Fuel Gauge for Aviation and Watercraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.599-602, June 2019, Available :http://www.jetir.org/papers/JETIR1908085.pdf

"Calibration and Volumetric Measurement of Fuel Gauge for Aviation and Watercraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp599-602, June 2019, Available at : http://www.jetir.org/papers/JETIR1908085.pdf