Investigation of the Accuracy of Barometric Pressure Sensors to Assessment of Their Possibility for UAVs Landing

This paper describes the results of the simulation of an absolute pressure sensor, which is used as a flight altitude meter, provided that its readings are corrected based on measured values of air humidity and ambient temperature. The simulation is performed using a virtual project of an altimeter created in the LabVIEW program, to which the test set of the specified sensors is connected.