The system is suits the controlled plants with pure delay property especially. It can restrain the oscillation of the system.
该系统特别适合那些具有纯滞后特性被控对象的控制，有效抑制系统振荡。
For nonlinear attitude system of flying vehicle with pure time-delay, inertia and bang-bang control a control method using decoupling variable structure is given.
对于具有纯延迟、惯性和由开关控制的非线性飞行器姿态系统，本文提出了采用解耦变结构控制的方法。
Holds that by this way the influence of the large pure delay on the system stability can be overcome.
认为该方法能有效克服大纯滞后对控制系统稳定性的影响。
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