This paper presents an iterative method for separating singular perturbation control systems.
文章提供了一种奇异摄动控制系统的迭代分解方法。
Based on the singular perturbation theory, the flight control system of MRV was divided into two loops, and the TLC controllers were designed for both loops.
基于奇异扰动原理，将MRV飞行控制系统分为内外两个回路，并且为两个回路都设计了轨迹线性化控制器。
On the basis of singular perturbation approach, the controller consists of a NN slow subsystem and a robust-based fast control subsystem.
根据奇异摄动方法，该控制器包括一个神经网络缓慢子系统以及强大的快速控制子系统。
In addition, the semi-active adaptive control law, based on singular perturbation analysis, can better decrease vibration of the system and meet the engineering requirement.
论文同时也验证了基于奇摄动理论设计的控制方法能够更好地抑制斜拉索振动，满足工程控制要求。
Towards 3 dimension(3D) air combat, forced singular perturbation is used to tackle the problem of pursue-escape strategies and the sub-optimal fire control model is built.
针对三维空战，应用强迫奇异摄动理论解决了追逃最优策略无法求解的难题，建立起了三维中距空战的追逃次最优火控模型。
Towards 3 dimension(3D) air combat, forced singular perturbation is used to tackle the problem of pursue-escape strategies and the sub-optimal fire control model is built.
针对三维空战，应用强迫奇异摄动理论解决了追逃最优策略无法求解的难题，建立起了三维中距空战的追逃次最优火控模型。
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