• 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得到侧滑虚拟传感器信号非线性观测器方法利用INSGPS系统数据估计迎角和侧滑角方法。

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  • In terms of the aircraft characteristics, the aircraft dynamics are divided into fast dynamics of Angle speeds and slow dynamics of roll Angle, Angle of attack and sideslip Angle.

    根据飞机动态特性飞机动态分为角速度快速动态转角、迎侧滑角表示的动态。

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  • For the aircraft with moderate swept wing, the main reasons of causing wing rock are the variations of roll damping moment with the Angle of attack and the sideslip Angle.

    具有中等后掠角机翼飞机产生机翼摇晃主要原因滚转阻尼力矩随迎侧滑角的变化

    youdao

  • For the aircraft with moderate swept wing, the main reasons of causing wing rock are the variations of roll damping moment with the Angle of attack and the sideslip Angle.

    具有中等后掠角机翼飞机产生机翼摇晃主要原因滚转阻尼力矩随迎侧滑角的变化

    youdao

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