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Existence of Gaps on the Path of Equilibriums in Case of Longitudinal Flight with Constant Forward Velocity

机译:恒定向前速度纵向飞行情况下平衡路径上的间隙的存在

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In this paper it is shown that, in case of longitudinal flight with constant forward velocity of the aircraft considered in [1], on the path of equilibriums there exist gaps and two pieces of the paths are removed. These gaps are hidden when the path of equilibriums is computed by using the decoupled system of three differential equations[1]. That is because the decoupled system is well defined for any value of the Euler pitch angle. The complete system of nine differential equations, from which the system of three differential equations was decoupled, is well defined only for the values of the pitch angle situated in the open interval (-π/2,π/2) . Here first the equilibriums reported in [1] for which the pitch angle is equal to -π/2 or π/2 are removed from the paths and so on the paths gaps appear. After that the equilibriums for which the pitch angle is not in the open interval -π/2,π/2) are also removed. It is shown that according to the complete system if the elevator deflection takes a value corresponding to a gap, then the aircraft exhibits jump phenomenon.
机译:在本文中,示出了,在[1]中考虑的飞机的恒定前向速度的纵向飞行情况下,在均衡的路径上存在空隙,并且去除两条路径。当通过使用三个微分方程的解耦系统计算均衡路径时,隐藏这些间隙[1]。这是因为对于欧拉桨距角的任何值,解耦系统很好地定义。九个微分方程的完整系统,三个微分方程的系统已经分离,仅针对位于打开间隔(-π/ 2,π/ 2)中的俯仰角的值很好地定义。此处首先,在[1]中报告的平衡角度等于-π/ 2或π/ 2,从路径上移除,因此出现在路径间隙上。之后,还去除了俯仰角不在打开间隔 - π/ 2,π/ 2)的平衡。结果表明,根据整个系统,如果电梯偏转采用与间隙对应的值,则该飞机表现出跳跃现象。

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