The above methods also apply to analysis of calculating stability for general linear equation group.
该方法也适用于分析一般线性方程组求解的稳定性。
To solve circuit analysis is getting for solution of corresponding real number or complex number linear equation group.
解决电路分析问题就是求解相应的实数或复数线性方程组。
Then, the basic solution set of conical magnetic bearing static operation points is given based on the solution structure of linear equation group.
由非齐次线性方程组解的结构给出静态工作点的基础解；
Based on the upper discussions, a new solution is presented which skipped the calculation of the ray and acquired the locating point by a linear equation group.
根据分析提出了新的方案，新方案中跳过了射线的计算，直接通过线性方程组得到定位点。
The nonlinear equation group expressed by infinite series was made up in the condition of different water level and recharge quantity on two lateral linear recharge boundary.
对于两侧直线补给边界水位和补给流量不同的情况，建立了无穷级数表达的非线性方程组；
The composed programme USES successive substitution method to solve nonlinear equation group, and provides the influence distance conception of the linear recharge boundary and method to determine it.
编制的计算程序用叠代法求解非线性方程组；并提出直线补给边界影响距离概念和确定的方法。
Based on the absorbance data of a group, standard solution, working equation of component was established by linear regression.
根据一组已知浓度混合液的吸光度，经一无线性回归建立组分的工作方程。
It is shown that for some relatively simple conditions, exact analytical solutions of the non linear consolidation equation can be obtained by using the approach of the transformation of Lie group.
研究表明，对于一些相对简单的边界条件，通过李群变换的方法可以得到非线性固结方程的完整解析解。
The dynamic equation of motion chain is a group of high non-linear differential equations, the solution is difficulty.
锚泊线的运动方程是一组高非线性的偏微分方程组，求解困难。
Bistable optical devices modulating function and clectro- optical feedback function are a group of non- linear equation.
光学双稳态的调制函数和反馈函数构成一组非线性方程。
This paper describes the relationship between the rank of matrix, the rank of vector group and liner equation group in the linear algebra.
讨论了线性代数中矩阵的秩、向量组的秩与线性方程组的秩之间的关系。
Features about the controlled object, helicopter, are first introduced briefly and a group of six free-degree, linear motion equation in combination with micro disturbance and couple are established.
首先对被控对象之一的直升机的特性进行了简单介绍，建立了直升机六自由度线性小挠动方程。
Features about the controlled object, helicopter, are first introduced briefly and a group of six free-degree, linear motion equation in combination with micro disturbance and couple are established.
首先对被控对象之一的直升机的特性进行了简单介绍，建立了直升机六自由度线性小挠动方程。
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