The invention provides a
simulation method for a four-rotor aircraft, and relates to a real-time
simulation method of an unmanned aircraft. The
simulation method for the four-rotor aircraft solves the problems that an existing semi-physical
simulation system is huge in size, complex in connection, low in accuracy due to the fact that
virtual state variables exist in simulation, and low in accuracy of a model obtained through modeling applying a
controller design method based on the models and a numerical
simulation system mechanism, wherein the
controller design method based on the models and the numerical
simulation system mechanism cannot be applied to modeling easily. According to the simulation method for the four-rotor aircraft, the actual aircraft is regarded as the controlled object and connected to a simulation circuit, and a reference is provided for the numerical simulation models obtained by mechanism modeling in
MATLAB / Simulink, so that accuracy of aircraft mechanism modeling can be verified rapidly. A parameter recognition method is adopted so as to guarantee accuracy of objective models in numerical simulation, so that feasible controllers are verified in the numerical simulation and the controllers can be finally effectively applied to actual physical objects. The simulation method for the four-rotor aircraft is specifically applied to the field of four-rotor aircraft simulation.