A vibration-controlled device with paired inclined nozzles is designed to reduce the barrel vibration and minimize the im? pact on the aircraft during continuous firing. The newly designed paired inclined nozzles generate only dynamic moment and recoil force， without producing transverse force. An interior ballistics model of the barrel with lateral channels is established， and the TVD-MacCormack difference scheme is utilized to numerically calculate the flow field in the barrel and the time-dependent aerody? namic force of the nozzles. Dynamic simulations of the continuous firing process of the aircraft gun are conducted to evaluate the ef? fect of the paired inclined nozzles on the muzzle vibration. Results show that the time difference of the maximum aerodynamic force of the two nozzles is 0.07 ms， with a relative difference of the maximum aerodynamic force of only 0.5%. This indicates that the two nozzles are well synchronized. The paired oblique nozzles can greatly reduce the muzzle vibration without compromising the ini? tial velocity of the projectile. The linear displacement and velocity of the lateral vibration decrease by 26.9% and 44.3%， respec? tively. The recoil momentum also decreases by 17.93%， without generating transverse force on the aircraft. As a result， the impact on the aircraft is significantly reduced. The achievements of this research will support the design of aircraft gun barrels with paired inclined nozzles