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,對新一代殲擊機超機動飛行的非線性模型的開環特性、分叉特性及機動能力進行分析,并以此模型為基礎,采用基于時標分離原則的動態逆控制方法設計了新一代殲擊機的飛行控制系統。