The invention provides a wing gust mitigation control method based on combined
plasma excitation, and belongs to the technical field of aircraft gust mitigation control. The control method comprises the following steps: S1, acquiring an aerodynamic characteristic curve of the wing; s2, a first installation position is determined based on the aerodynamic characteristic curve obtained in the step S1, and a first
plasma exciter is installed at the first installation position; s3, determining a second mounting position based on the aerodynamic characteristic curve obtained in the step S1, and mounting a second
plasma exciter at the second mounting position; and S4, a gust
signal of the wingtip or the
nose of the unmanned aerial vehicle is obtained, and the first plasma
exciter or the second plasma exciter is controlled to operate according to the gust
signal. Induced
jet flow is generated on the surface of the wing through the plasma exciter and acts on an
airflow field on the surface of the wing,
aerodynamic force fluctuation of the wing is controlled, gust load is slowed down, and hang time is prolonged.