The invention belongs to the technical field of aircraft
simulation, and particularly relates to a flight
simulation method and device under gust load. The method comprises the following steps: S1, carrying out 1g
level flight balancing on the aircraft, and determining a balancing
attack angle of the aircraft and a balancing
elevator skewness of the aircraft; s2, determining the
aerodynamic force of the aircraft; s3, dynamic response solving is conducted on
aerodynamic force of the aircraft, the aerodynamic
attack angle, the
flight speed and the
pitch angle speed are obtained, and normal overload of the aircraft is determined after the
flight speed is superposed with the
wind speed of the vertical gust field; s4, acquiring the
elevator skewness calculated by the stability
augmentation system, and superposing the
elevator skewness at the previous
simulation moment to obtain the actually required elevator skewness; and S5, re-determining the
aerodynamic force of the aircraft according to the
flight speed, the
pitch angle speed, the aerodynamic
angle of attack and the actually required elevator skewness until the simulation is finished. The effect of the stability
augmentation system in the determination process of the gust load of the aircraft is considered, the simulation process is simple, and the precision is high.