First, the SISO case is developed and applied to the adaptive control of the fight path Angle of an aircraft.
首先，对于单输入单输出情况，将其用于飞行器飞行路线角的自适应控制。
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。
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。
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。
应用推荐