• By introducing state transformation, a reduced-order state estimation form is achieved.

    通过引入状态变换,得到了一类降阶形式的状态估计问题。

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  • A state transformation method is applied to analyze quantitatively several logical structures of fuze safety systems.

    采用状态转移法对引信安全系统的几种逻辑结构进行了定量的安全性分析。

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  • The state transformation is used to convert a system with uncertain and unmatched input time-delay into a delay-free one, with a sliding mode controller designed.

    针对具有输入时滞、且同时具有非匹配不确定项的一类对象模型,采用状态变换法把原系统转化成为一个无时滞系统,并应用滑模控制的方法设计了控制器。

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  • The observer design problem for general nonlinear multi-input and multi-output system by nonlinear state transformation is studied. The observer design conditions and method are generalized.

    研究一般的非线性多输入多输出系统状态观测器的设计问题,采用状态非线性变换讨论了这种观测器的设计方法及条件。

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  • Thus by nonlinear state transformation and nonlinear state feedback, the original 6 order nonlinear attitude model of a spacecraft is partially precisely linearized into a 2 order linear system.

    这样通过非线性状态变换和非线性状态反馈,将飞行器原来的6阶非线性姿态模型部分精确线性化为二阶线性系统。

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  • Thus by nonlinear state transformation and nonlinear state feedback, the original 6 order nonlinear attitude model of a spacecraft is partially precisely linearized into a 2 order linear system.

    这样通过非线性状态变换和非线性状态反馈,将飞行器原来的6阶非线性姿态模型部分精确线性化为二阶线性系统。

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