The flutter active controller design based on receptance method can obtain the corresponding model parameters based on the experimental model and carry out the controller parameter solving. However, the current controller design based on receptance method ignores a large number of coupling terms of the aerodynamic servoelastic model, resulting in low applicability of the controller. In this paper, the AGARD wing aeroservoelastic model is taken as the object to construct the aeroservoelastic model including the coupling effect of the control surface. A receptance method based on the active flutter controller design considering the coupling effect of the control surface is proposed, and compared with the original controller.Finally, the controller parameter fitting is studied at any incoming flow velocity. The simulation results show that the controller designed by the original method is difficult to be applied to the aeroservoelastic model with the influence of control surface coupling. However, the new receptance method active flutter controller derived in this paper can accurately configure the characteristic roots of the closed-loop system to meet the design requirements. The active flutter controller with fixed parameters is designed at a design point lower than the open-loop flutter speed, which can increase the flutter pressure by 30%.