Reduction of the Influence of Interfering Signals on the Longitudinal Control of UAVs with Fixed Wing

Table 5

Standard deviation values of the noise introduced into the measurement by the UAV engine.

Sensor axis
Accelerometer (m/s)		0.0547927
		0.0495273
		0.0741763
Gyroscope (°/s)		0.0032016
		0.0017807
		0.0020208