This thesis designs an inertial controlling method to the height with the signal of the axis apparent acceleration and its integral by the method of conjugate equation.
本文以飞行器轴向视加速度及其积分为控制信号，用共扼方程法设计了一种惯性高度控制方法。
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Acceleration along each axis is reported directly by the hardware as G-force values.
沿着每个轴的加速度由硬件作为G - force值直接报告。
3
Objective To explore the effect of different axial (x or Y axis) radial acceleration on Coriolis illusion.