The invention particularly relates to a pulse Doppler echo
simulation method for a rotor unmanned aerial vehicle, which comprises the following steps: enabling a
fuselage to be equivalent to an isotropic scattering point, and simulating a
radar echo signal of the
fuselage based on the RCS of the scattering point of the
fuselage and the distance between a
radar and the
gravity center of the fuselage; rotor blades are equivalent to a group of isotropic scattering points uniformly distributed on a straight line, and
radar echo signals of the rotor scattering points are simulated based on the RCS of the rotor scattering points and the distance from the rotor scattering points to the
gravity center of the fuselage; simulating a radar
echo signal of a single blade based on the radar
echo signal of the rotor wing scattering point, simulating a radar echo
signal of a single rotor wing based on the radar echo
signal of the single blade, and simulating radar echo signals of all rotor wings based on the radar echo
signal of the single rotor wing; and simulating a pulse Doppler echo signal of the rotor unmanned aerial vehicle based on the radar echo signals of all the rotors, the radar echo signal of the fuselage and the echo signal
noise. According to the method, the radar echo characteristics of the rotor unmanned aerial vehicle are simulated more truly.