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。
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