In most flight conditions it is desired to maintain the sideslip angle equal to zero . 大多数飞行状态都要求保持侧滑角等于零。
Both the sideslip angl e and the rudder angle are seen to be very much dependent on the angle of climb . 人们可以看到,侧滑角和方向舵偏角都在很大程度上依赖于爬升角。
This paper introduces two methods to get the virtual sensor signal of angle of attack and sideslip angle : nonlinear observer method and ins / gps method 本文介绍了两种方法来得到迎角和侧滑角的虚拟传感器信号:非线性观测器方法和利用ins gps系统数据估计迎角和侧滑角方法。
The pressure model of flush airdata sensing system is nonlinear equations of the angle of attack , angle of sideslip , dynamic pressure and static pressure of the free stream 飞行器表面的压力分布是大气数据(迎角、侧滑角、动压、静压)的非线性函数,这个函数主要可以从空气动力学模型得到。
The relevance functions between total pressure recover coefficient and the parameters ( mach number , angle of attack , flow coefficient , angle of sideslip ) for subsonic submerged inlet in turbojet and turbofan engine were investigated 摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式,表现为关于马赫数、流量系数、攻角、侧滑角的函数。