提出了一种飞机大仰角飞行的动态逆模糊集成控制方法。

This paper presents a dynamic inversion control method for high Angle - of - attack flight.

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梯度使气流方向测量值向负梯度方向偏转。 圆柱探针和锥形多孔探针相比，气流方向测量误差对速度梯度更敏感，纵向梯度对俯仰角测量值的影响尤其大。

The velocity gradient, especially the perpendicular velocity gradient, leads the measuring error of flow angle with cylindrical probe to be larger than with conical multi-hole probe.

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