当不计飞行器的响应时间、纵向加速度和控制溢出时，蜕化为常规比例导引。
Neglecting the time canstants, axial accelerations and the control overflow, the optimal strategy is reduced to the conventional proportional navigation guidance law.
对一个单自由度结构有CTLD控制和无ctld控制时的加速度响应进行了精确数值求解，结果验证了CTLD能够有效地控制结构在地震作用下的加速度响应。
It is shown from pure numerical simulations for a SDOF system with and without CTLD control that the CTLD can effectively control the acceleration response of a structure.
提出了基于横摆率跟踪控制的4ws和主动悬架的协调控制方法，对前后轴主动悬架控制力进行了分配，提高了大侧向加速度时的横摆率响应。
A coordinated control scheme of 4ws and active suspension based on yaw rate tracking is proposed, which distributes the control force between front and rear active suspensions and hen.
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