DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.
介绍了将DMC - PID串级控制技术应用到无人机无动力飞行时的自动着陆阶段迎角自动控制系统。
In view of the weak nonlinearity and time-delay characteristics of AMT clutch engagement position control system, DMC-PID cascade predictive control algorithm is applied to the system.
针对AMT离合器接合位置控制系统具有的时滞弱非线性特性，采用DMC-PID串级预测控制算法应用于该系统。
This scheme overcomes the shortcomings of pure PID control and the pure DMC arithmetic whose single structure causes poor inner anti-jamming ability.
它既克服了单纯PID鲁棒性差的缺点，又克服了单纯DMC由于单层结构而带来的抗内扰能力弱的问题。
Compared with the PID algorithm, the DMC algorithm has the obvious advantages in processing the time-delay objects.
DMC算法在处理时滞对象时与PID算法相比具有明显的优点。
Therefore the control quality is superior to that of the conventional PID or DMC.
其控制品质优于常规的PID和一般的DMC控制。
In succession, the paper introduces the control algorithms used in experiment, which include PID control, fuzzy logic control, DMC predictive control and relay feedback identification.
这是因为在相关实验中的控制器算法设计在基本原理上具有一致性。所应用的控制算法包括PID、模糊、DMC预测控制以及对象过程特性的继电反馈辨识。
In succession, the paper introduces the control algorithms used in experiment, which include PID control, fuzzy logic control, DMC predictive control and relay feedback identification.
这是因为在相关实验中的控制器算法设计在基本原理上具有一致性。所应用的控制算法包括PID、模糊、DMC预测控制以及对象过程特性的继电反馈辨识。
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