1) estimation of angle-ofattack and sideslip-angle
迎角和侧滑角估计
2) angle of attack and sideslip
迎侧角
3) Estimation of the trigonometrical sum
三角和估计
5) sideslip angle
侧滑角
1.
Detection system of aero attack and sideslip angle sensor;
飞机攻角侧滑角传感器检测系统
2.
For several reasons, the angle of attack and the sideslip angle cannot be measured accurately especially when angle of attack is high.
针对迎角和侧滑角,特别在大迎角飞行情况下不能够精确测量的问题,研究了一种利用INS/GPS系统数据结合其他辅助系统来估计迎角和侧滑角的方法,利用INS/GPS系统测量的地速和总加速度信号结合飞机其他传感器和数学模型估计得到了迎角和侧滑角传感器的虚拟信号。
3.
It s the effect of sideslip angle on aerodynamic interactions between rotor/fuselage,rotor/horizontal tail and rotor/ vertical tail that is especially discussed.
介绍了一副研究型马赫数相似旋翼和 Z9机身组合模型低速风洞的试验概况 ,着重讨论了侧滑角对旋翼 /机身、平尾及垂尾气动干扰特性的影响。
6) angle of sideslip
侧滑角
1.
Calibration of angle of sideslip using fuzzy neural network;
模糊神经网络的侧滑角校正
2.
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。
补充资料：侧滑角传感器
见迎角传感器。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条