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。
So the author improves the 2-d sector filtering method, introduces the bang-transit and cake-cut filtering method in frequency - wave count area.
因此,作者将二维扇形滤波方法做了近一步的改善,引入了频率—波数域内带通切饼式滤波方法。
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