The signal of the pitch integral and the pitch acceleration sensor (here red and yellow) should show a significant value.

俯仰积分和俯仰加速度传感器信号(以红色和黄色表示)应该表现出显著的值。

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Data about the airspeed, altitude, pitch, acceleration, roll, fuel, and the list goes on and on.

这些数据包括飞行速度、高度、俯仰、加速度、晃动、燃油等情况。

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So, variable structure control theory is used in Angle stabilization of roll, and model - following variable structure control theory is used in acceleration stabilization of pitch and yaw.

因此，本文采用了变结构控制理论设计倾斜角稳定系统，采用了模型跟踪变结构控制理论设计俯仰、偏航通道的加速度稳定回路。

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So, variable structure control theory is used in Angle stabilization of roll, and model - following variable structure control theory is used in acceleration stabilization of pitch and yaw.

因此，本文采用了变结构控制理论设计倾斜角稳定系统，采用了模型跟踪变结构控制理论设计俯仰、偏航通道的加速度稳定回路。

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