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。
Because the temperature control system is a pure time delay system which will cause system unstable or reduce work performance.
由于温度控制系统为纯滞后系统，纯滞后会引起系统的不稳定或降低系统的工作性能。
Because the temperature control system is a pure time delay system which will cause system unstable or reduce work performance.
由于温度控制系统为纯滞后系统，纯滞后会引起系统的不稳定或降低系统的工作性能。
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