Table 1 The simulation parameters of the environment

Speed of light c

\(3 \times {10^8}\) m/s

Channel bandwidth B

150 MHz

Carrier frequency \(f_c\)

30 GHz

Pilot duration ratio \(T_{p}/T\)

\(2\times {10}^{-4}\)

Thermal noise power density

-174 dBm/Hz

Tip speed of the blade \(U_{t}\)

60 m/s

Mean induced speed \(v_{0}\)

2.486 m/s

lade profile power \(P_{0}\)

112.203 W

induced power \(P_{1}\)

10.574 W

Fuselage drag proportion \(d_{0}\)

0.5

Air density \(\rho\)

1.225 \(kg/m^{3}\)

Rotor solidity s

0.0832

Rotor disc area A

0.2827 \(m^{2}\)