This paper discussed the application of this method in the design of flight control system for the post stall maneuver.
针对过失速机动飞机探讨了非线性动态逆方法在飞行控制系统设计中的应用。
Study of the mechanism, prevention and recovering methods of stall and spin for supersonic fighter is a important means to improve battle ability and keep a safe flight.
研究超音速飞机失速和尾旋的机理预防和改出方法，是提高超音速战斗机作战能力和保障飞行安全的重要手段。
Taking the flight parameters of F-15 fighter as analysis background, the affection of stall and thrust vector on instantaneous turning performance is studied.
以F - 15战斗机为例，研究了失速及推力矢量对飞机瞬时转弯性能的影响。
Based on the analysis of typical post-stall maneuvers, steady linear flight, rapid pitching and rolling about velocity vector are presented as three typical basic movements.
对典型过失速机动的运动特性进行了分析，根据其运动特点将过失速机动的运动过程分解为定直飞行、快速俯仰和绕速度矢量旋转三种基本运动的组合。
The locating, installation and calibration of stall warning device are all determined by the experiment in flight test.
失速警告器的选位安装与校准均由试飞实验确定。
The locating, installation and calibration of stall warning device are all determined by the experiment in flight test.
失速警告器的选位安装与校准均由试飞实验确定。
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