First of all , it is devoted to discuss the open - loop characteristics and the nonlinear bifurcation analysis and the maneuver ability for the super - maneuverable flight nonlinear model of the new generation fighter . then a flight control system is designed in analytical dynamical inversion method based on the time - scale separation principle 首先,对新一代歼击机超机动飞行的非线性模型的开环特性、分叉特性及机动能力进行分析,并以此模型为基础,采用基于时标分离原则的动态逆控制方法设计了新一代歼击机的飞行控制系统。