1) local linear method
局部线性方法
1.
In this paper,estimations of varying-coefficient models with the correlated random errors are given by the local linear method.
在误差相关的情况下,使用局部线性方法给出变系数模型的估计,并讨论估计的渐近正态性。
2.
The estimate of the unknown coefficient functions is proposed by local linear method,and the estimate of the unknown parameters is given by least-square technique,and asymptotic normality of the estimation is investigated.
先用局部线性方法给出未知系数函数的估计,再由最小二乘法估计出未知参量,并讨论了估计的渐近正态性。
3.
First,with the local linear method,the coefficient functions of the model are estimated,and then,with the integration method,their integrations are estimated.
首先,使用局部线性方法给出模型的系数函数的初始估计;然后使用积分方法,给出它们的积分估计;进一步,研究这些积分估计的渐近正态性。
2) adaptive local linear method
自适应局部线性化方法
3) local linearization method
局部线性法
1.
Three parameters, which are the delay time of load record series, embedded space dimension and distance in choosing the neighboring points, need to be determined in forecasting short term loads by the local linearization method of phase space reconstruction.
采用混沌方法中相空间重构法的局部线性法进行短期负荷预测时 ,需要优选 3个参数 ,即负荷记录序列的延时时间、嵌入相空间的维数以及选择邻近点时使用的距离。
4) local/methods
局部/方法
5) local approach
局部方法
1.
Fault detection for inertial measurement unit based on local approach;
基于局部方法的余度惯性组件故障诊断
6) local method
局部方法
1.
The local method with the regimecoefficients derived from shock tunnel experimental results for oneconfiguration was applied to predicting the aerodynamic force coeffi-cients for the another configuration.
应用局部方法以一种迎风面外形的实验结果为依据,估算了另一迎风面外形的气动特性,结果与实验值吻合较好。
2.
The paper widens the application of local method which used to be utilized in rarefied flow to the quick prediction of aerodynamic characteristics of missile-like reentry vehicle in hypersonic flow.
本文将计算高超声速稀薄气流过渡领域中气动特性的局部方法,推广应用到连续介质中弹头型高超声速再入飞行器气动力特性的快速估算。
补充资料：局部一维方法
见分步法。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条