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

Table 1

The UAV’s aerodynamic coefficient values obtained by simulation.

Effects		Shortcut	Dependency on variable	Value
Aerodynamic coefficients of forces	Axis		Dependency of lift on	4.56
			Dependency of lift on	0.51
			Dependency of lift on	-0.85
		𝐶𝐿_𝑞	Dependency of lift on	7.2
	Axis		Dependency of drag on	0.39
			Dependency of drag on	0.03
	Axis		Dependency of side force on	-0.18
			Dependency of side force on	0.314
			Dependency of side force on	0.2
Aerodynamic coefficients of moments	Axis		Dependency of roll moment on	0.004
			Dependency of roll moment on	-0.1
			Dependency of roll moment on	0.012
			Dependency of roll moment on	-0.32
			Dependency of roll moment on	0.028
	Axis		Dependency of pitch moment on	-2.442
			Dependency of pitch moment on	-48
			Dependency of pitch moment on	-1.13
			Dependency of pitch moment on	-0.04
	Axis		Dependency of yaw moment on	-0.09
			Dependency of yaw moment on	-0.07
			Dependency of yaw moment on	-0.12
			Dependency of yaw moment on	-0.04
			Dependency of yaw moment on	0.089