• This paper presents a computer simulation model of the cardiovascular circulation system, which describes the blood flow dynamic law in the cardiovascular system by the state equation.

    建立一种心血管循环系统的计算机仿真模型,即描述心血管循环系统内血流动力学变量变化规律的状态方程。

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  • Based on state equation for structural dynamic response, the iteration computing scheme is established.

    基于结构动力响应分析的状态方程,建立了迭代计算格式。

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  • The molecular dynamic data of compressibility factor are used to regress this two localized radial distribution functions. Therefore, a new equation of state of square well fluids is established.

    利用已知的压缩因子分子动力学模拟数据,回归得到了这两个径向分布函数,从而建立了一个新的方阱流体状态方程。

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  • The main idea of Kalman filtering is to describe the linear dynamic system using state equation and measurement equation.

    卡尔曼滤波的主要思想,是用状态方程和量测方程描述线性动态系统。

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  • Based on bond graph theory, the bond model of a road smoothness measuring equipment vibration has been set up, and the state equation and the dynamic simulation program established.

    应用键合图理论建立了路面平整度仪振动系统的键合图模型,并推导出状态方程,编制了动态仿真程序。

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  • For the dynamic system with the measurement equation and state equation, the robust FDD approach is discussed.

    对基于系统量测方程和状态方程的动态系统,研究了系统的鲁棒故障检测与诊断(FDD)问题。

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  • Using the extreme state of dynamic tension equation, the steady tension and shock peak value can be calculated.

    利用动态方程的极限状态,求出稳定平衡后的张力和上冲峰值。

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  • The dynamic performance of synchronous motor under abrupt change of load is investigated using the state equation.

    利用同步电动机的状态方程,研究了同步电动机在突加负载时的动态过程。

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  • In the time domain analysis of dynamic circuit, the initial state must be first known when the differential equation or state equation will be solved.

    在动态电路的时域分析中,若要解出描述电路的微分方程或状态方程,首先必须知道电路的初始状态。

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  • A kind of Bayesian dynamic model with nonlinear state equation is solved by Tierney and Kadane 's approximate computation.

    对一类非线性动态模型,利用帝尔尼和卡登近似对模型进行了模拟计算。

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  • Aircraft longitudinal dynamic response of the system with and without LEX is analyzed by solving the state equation of aircraft longitudinal motion.

    通过求解全机纵向运动状态方程,分析了全机模型带与不带机翼边条时纵向动态响应问题。

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  • To start with, the system dynamic equation is transformed into discrete-time state equation in observable canonical form.

    首先,将系统动力学方程转化为离散的可观标准型状态方程;

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  • To start with, the system dynamic equation is transformed into discrete-time state equation in observable canonical form.

    首先,将系统动力学方程转化为离散的可观标准型状态方程;

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