Table 2.

Simulation parameters.

Parameter	Value
Blade profile power $\left(P_0\right)$	80 W
Induced power $\left(P_i\right)$	88.5 W
Tip velocity of rotor blade $\left(U_{tip}\right)$	120 m/s
Average rotor induced velocity at hover $\left(v_0\right)$	4.03 m/s
Airframe resistance ratio $\left(d_0\right)$	0.6
Air density $\left(\rho \right)$	1.225 kg/m${}^3$
Rotor firmness $\left(s\right)$	0.05
Rotor disk area $\left(A\right)$	0.503 m${}^2$
Contour resistance coefficient $\left(\delta \right)$	0.012
Blade angular velocity $\left(\mathsf{\Omega }\right)$	300 rad/s
Rotor radius $\left(R\right)$	0.4 m
Rotor thrust increment correction coefficient of induced power $\left(k\right)$	0.1
UAV weight $\left(W\right)$	20 N
Launch power of UAV $\left(P_U\right)$	37 dBm
System available channel set $\left(L\right)$	50
Channel power gain at 1 m $\left(\beta \right)$	−75 dB
Noise power $\left(N_0\right)$	−104 dBm
UAV flying altitude $\left(H\right)$	100 m
UAV coverage radius $\left(R\right)$	300 m
System bandwidth $\left(B\right)$	1 MHz
Data information threshold $\left(Q\right)$	15 Mbit
UAV hovering time $\left(T_h\right)$	120 s
Communication-related power $\left(P_t\right)$	5 W