可供从事过失速飞行试验战术机动研究的技术人员和飞行人员参考。
It will give a reference to technicians and flight crew engaging in flight test research of post tall and tactical maneuver.
可供从事过失速飞行试验战术机动研究的技术人员和飞行人员参考。
It will give a reference to technicians and flight crew engaging in flight test research of post tall and tactic al maneuver.
可供从事过失速飞行试验、战术机动研究的技术人员和飞行人员参考。
It will give a reference to technicians and flight crew engaging in flight test research of post tall and tactical maneuver.
飞行专家质问为何飞行员面对飞机失速不是通过提起机头而是压制机身来恢复正常状态。
Aviation experts are asking why the pilots responded to the stall by pulling the nose up instead of pushing it down to recover.
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。
This paper discussed the application of this method in the design of flight control system for the post stall maneuver.
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。
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.
没有经验的飞行员很容易使他的飞机失速。
第二类，一个〝不对称的失速〞或者〝平转〞，只发生在当飞行员用双侧煞车减速，在将近失速点之前过度使用单侧煞车时。
The second type, an "asymmetric stall" or "flat spin happens when the pilot slows down on both brakes to just before stall point and then further applies one brake.
动态全失速是指当伞头在飞行员背后的时候进入全失速。
A dynamic full stall is performing a full stall when the glider is behind the pilot.
为了研究飞行器在纵向大迎角状态下的动态失速现象，设计了一套用于低速风洞的升沉振动测量装置。
In order to study dynamic stall phenomena of an aircraft in portrait at a high Angle of attack, designing a measuring device of heave oscillation for a low speed wind tunnel.
从飞机设计的角度分析了过失速机动飞行的操纵要求问题。
From the viewpoint of aircraft design, a topic on control design requirements for post stall maneuvering is tackled.
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。
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.
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverability wi…
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverabil…
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverability with satisfactory fl...
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverability with satisfactory fl...
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