失速控制，卸荷，手动电子刹车。
使用符号运算方法设计了系统闭环控制律和大攻角下的过失速控制律。
The control laws of the inner closed loop system and post stall maneuver are obtained through using symbol operations design.
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.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
虽然许多飞机设计往往拥有低失速速度，设计许多这些同样具有这些低效益的速度，最低程度的控制。
While many aircraft designs often boast a low stall speed, many of these same designs have minimal control effectiveness at these lower speeds.
本文对动失速型非定常分离涡结构的控制方法，在低速风洞中应用相平均测压技术进行了实验研究。
Experimental investigation on the control of dynamic stall type vortex flow was made in a low speed wind tunnel by using phase averaged pressure measurement technique.
本文对动失速型非定常分离流的主动控制方法在低速风洞中进行了实验研究。
An experimental investigation on the active control of dynamic stall type unsteady separated flow is carried out in the low speed wind tunnel using a phase averaged pressure measurement technique.
仿真结果表明，该控制律能控制推力矢量飞机顺利完成过失速机动，对系统模型的不确定性具有较强的鲁棒性。
The results show that the control law can control vectored aircraft to accomplish post-stall maneuvers very well and it is very robust to model uncertainty.
推力矢量控制技术和过失速机动使战斗机的空战效能大大增加，引起了世界各国的关注。
The thrust vectoring control technology and post-stall maneuverability enhance the aircraft's combat effectiveness greatly, and cause the worldwide interest.
为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。
The study will provide a new theoretical approach to investigate aircraft agility, the direct force control and post-stall maneuver of modern combat aircraft.
这时候要求我们稳定的控制操纵，并且在速度减小到失速速度之前使飞机低头，在满油门的情况下加速。
We ought to hold the column and make the aircraft nose down to accelerate with full poser before reach to the stall speed.
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 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 maneuverabil…
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