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。
At the same time, this control method has the good reference value to other object of big delay, variable parameter.
同时这种方法对其它的大滞后，特性参数不确定等控制对象的控制问题都有很好的参考价值。
Aiming at the networked control problem, a united model is established including variable network time-delay and data dropout, etc.
针对网络控制问题，建立包含变网络时延及网络传输丢包等的统一模型。
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