(National Aviation University, 2024-06-13) Duka, Yrii Serhiyovych; Дука, Юрій Сергійович
The use of a hydrostatic sensor in the fuel measuring system during maneuvering of the aircraft made it possible to achieve more accurate and reliable measurements in contrast to other methods of estimating the remaining fuel. The developed system allows you to effectively take into account the influence of various factors, such as pressure, temperature, flight altitude, changes in the position of the aircraft during movement on the determination of the remaining fuel. The results of the work can be used in the practical activities of airlines to optimize the fuel measuring system and improve flight safety. Further research can be aimed at improving technical solutions and expanding the capabilities of the system in different operating conditions of the aircraft.
