以放宽静稳定性（ＲＳＳ）战斗机Ｆ－１６为例，讨论了深失速走廊特性。利用具有非线性气动力的简化运动方程，分析了飞机深失速特性；应用反向积分技术确定出了深失速走廊——深失速平衡点的收敛区域（ＲＯＣ）。并分别对开环俯仰拉起和带过载滚转中惯性耦合引起的深失速进行了分析。最后阐述了一种改出深失速的非线性开关控制律。 Taking the F-16, the static relaxation (RSS) fighter, as an example, the characteristics of deep stall corridors are discussed. The simplified motion equation with nonlinear aerodynamic force was used to analyze the characteristics of deep stall of aircraft. The reverse integral method was used to determine the convergence region (ROC) of the deep stall corridor-deep stall equilibrium point. And the deep stall caused by the inertial coupling in the open-loop pitch pull-up and the belt overload roll are respectively analyzed. Finally, a nonlinear switch control law with a deep stall is introduced.