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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An inertial controlling scheme to the altitude with the signal of the axis apparent velocity and its integral by the method of conjugate equation is presented in this paper.