Open AccessDesign and Simulation of Air-Fuel Percentage Sensors in Drone Engine Controlling
Author(s) -
Mohammed Abdulla Abdulsada,
Mohammed Wajeeh Hussein,
Jabbar Shatti Jahlool,
Majid S. Naghmash
Publication year - 2022
Publication title -
trends in sciences
Language(s) - English
Resource type - Journals
ISSN - 2774-0226
DOI - 10.48048/tis.2022.1713
Subject(s) - automotive engineering , aircraft fuel system , fuel injection , drone , engineering , fuel efficiency , interface (matter) , fault (geology) , takeoff and landing , control system , fuel tank , matlab , jet engine , injector , simulation , computer science , mechanical engineering , aerospace engineering , electrical engineering , vapor lock , combustion chamber , pulmonary surfactant , chemistry , gibbs isotherm , biology , genetics , operating system , combustion , organic chemistry , chemical engineering , seismology , geology
This paper presents the design and simulation of air-fuel percentage sensors in drone engine control using Matlab. The applications of sensor engineering system have been pioneer in technology development and advancement of automated machine as complex systems. The integration of drone fuel sensor system is the major series components such as injector, pumps and switches. The suggested model is tuned to interface drone fuel system with fuel flow in order to optimize efficient monitoring. The sensor system is improved and virtualized in Simulink block set by varying the parameters with high range to observe the fuel utilization curves and extract the validated results. The obtained results show that the possibility of engine operation in critical conditions such as takeoff, landing, sharp maneuver and performance is applicable to turn off the system in case of break down in the sensor to ensure the safety of drone engine.
HIGHLIGHTS
The drone engine fuel rate sensor is designed and examined to determine the air-to-fuel ratio
The suggested model is tuned to interface drone fuel system with fuel flow in order to optimize efficient monitoring
The obtained results show that the possibility of using engine with different failure mode and fault considerations
The represented control structure is simple, efficient and provides the required air-to-fuel ratio