在采用MIL-1797-STD有人驾驶飞机飞行品质规范检验某第三代战斗机飞行品质过程中,在计算鹊克准则(即瞬时峰值比、上升时间及有效时间延迟)时,认为通过利用高阶系统传递函数求出的时间响应特性得出的结果比通过求解由飞机及控制系统组成的微分方程得出的结果更合理;在计算尼尔-史密斯准则时,提出了一种利用优化技术确定该准则的驾驶员参数kp和补偿τp1,τp2值的方法,取得了满意的效果。 When using the MIL-1797-STD pilot flight quality specification to test the flight quality of a third-generation fighter plane, the Magpie criterion (ie, instantaneous peak-to-peak ratio, rise time and effective time delay) The time response obtained from the transfer function gives a more reasonable result than the one obtained by solving the differential equation composed of the aircraft and the control system. In the calculation of the Neil-Smith criterion, an optimization technique is used to determine the criterion Driver’s parameter kp and compensation τp1, τp2 value method, and achieved satisfactory results.