A sliding mode observer is designed to estimate the Angle of attack and flight path Angle for a hypersonic vehicle.

对一个高超声速飞行器设计了滑动模态观测器来估计攻角和航迹倾角。

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After adopting the correcting method of flight path Angle, flight path planned is further modified and ideal reference flight path is obtained.

航迹角修正法的采用，进一步修正了规划出的飞行轨迹，从而获得了理想的飞行参考轨迹。

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After adopting the correcting method of flight path Angle, flight path planned is further modified and ideal reference flight path is obtained.

航迹角修正法的采用，进一步修正了规划出的飞行轨迹，从而获得了理想的飞行参考轨迹。

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