突风载荷减缓是改善飞机飞行性能的一项关键技术。基于紊流探测器获得的飞机前方突风速度信息,以翼根剪力、弯矩和翼尖加速度响应为减缓指标,建立了计入控制面偏转角度和偏转速率约束的突风载荷模型预测控制方法,设计了模型预测控制器,进行了闭环系统仿真,并与参考(PID)控制作了对比。仿真结果表明,模型预测控制能够有效抑制突风载荷。 Gob load reduction is a key technology to improve the flight performance of aircraft. Based on the information of the gust velocity in front of the aircraft obtained from the turbulence detector, the gust load model predictive control, which takes into account the constraints of the control plane deflection and the yaw rate, is established based on the blade root shear force, the bending moment and the tip acceleration response. Method, the model predictive controller is designed, the closed-loop system simulation is carried out and compared with the reference (PID) control. The simulation results show that the model predictive control can effectively suppress the gust load.