第一阶段研究美国空间控制系统的设计

Liu Xin, Quanmin Zhu, Pritesh Narayan, Yang Ye
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引用次数: 2

摘要

本研究提出了基于u模型原理的u状态反馈控制系统设计方法的基本思想。与基于u模型的非线性多项式系统相比,u状态空间设计是确定期望状态变量方程xd(t),从而求出控制器输出u(t-1)。期望状态方程可以很容易地设计/指定并转换为u状态空间表达式。通过求解方程可以得到控制器的输出。期望的状态变量由相应的状态变量x(t)更新。假设在本研究中状态变量是可测量的或由适当的观察者获得的。在实例研究中,选择了两个非线性离散时间状态空间模型来测试所提出的方法。计算实验,即仿真研究,证明了程序的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The first stage studies of U-state space control system design
In this study, a basic idea of U-state feedback control system design method is proposed based on U-model principle. Compared with U-model based nonlinear polynomial systems, the U-state space design is to determine the desired state variable equation xd(t), therefore to find the controller output u(t-1). The desired state equation can be designed/specified and transformed into the U-state space expression easily. The controller output can be obtained from resolving the equation. The desired state variables are updated by the corresponding state variables x(t). Assume that the state variables are measurable or obtained by a proper observer in this study. In case studies, two nonlinear discrete time state space models are selected to test the proposed approach. Computational experiments, that is, simulation studies, are used to demonstrate the procedure effectiveness.
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