本文采用(1-cosine)型离散突风,针对本机和B707机的起飞、爬升、巡航和着陆四个飞行阶段和各种航程及紊流情况,计算了开环系统和考虑驾驶员作用的闭环系统的各种响应特性。在求解各个响应量的变化过程时,采用了平移函数的概念,从而避免了冗长的积分运算和由积分步长带来的计算误差。依据Kpe~(τs)的驾驶员模型,着重考虑了K_p大小对响应量的影响,并认为在一般情况下采用中等水平的驾驶动作较为合适,而在着陆状态中,应采用更大的K_ρ才能抑止速度的沉浮特性。 In this paper, we use (1-cosine) discrete gusts. According to the four stages of take-off, climb, cruise and landing of the aircraft and B707, and the range and turbulence, the open-loop system and the driver's role Closed-loop system of various response characteristics. The concept of translation function is adopted in the process of solving the change of each response, which avoids lengthy integral calculation and calculation error caused by integral step. According to the driver model of Kpe ~ (τs), the influence of K_p size on the response is emphasized, and it is considered that it is more appropriate to use moderate level of driving maneuver in general, and larger K_ρ should be adopted in landing state Inhibit the speed of the ups and downs.