Using this method, the flight control law which suits to the vectored aircraft flight in post-stall domain is designed in this paper.3.
运用这种方法对推力矢量飞机进行了适用于过失速机动的非线性飞行控制系统设计。
参考来源 - 推力矢量飞机非线性飞行控制律设计研究The experiments showed that, with a steeped tip gap casing configuration, the compressor's total performances, both stable and post-stall performance, would be improved, if the casing had been properly configurated.
实验结果显示：如果梯状尖部间隙机匣处理的几何形状和几何尺寸——梯形周向槽的位置与深度——设计合理，则它不但可以改善压气机的稳态性能，还可以改善压气机的过失速性能。 所以，梯状尖部间隙机匣处理为机匣处理研究提供了一种新的研究方向，值得叶轮机械工作者对其开展进一步深入研究。
参考来源 - 新型机匣处理对轴流压气机过失速性能影响的研究·2,447,543篇论文数据，部分数据来源于NoteExpress
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.
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.
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