Script02

采用动态加权综合评价方法建立评价模型，增大了评价结果的客观性。首先对评价指标数据进行归一化处理，然后选取偏大型正态分布函数作为动态加权函数建立评价模型，从而对评价指标观测值进行排序，最后用决策(Dynamic weighted comprehensive uation method to establish uation model, increasing the objectivity of uation results. First uation data normalization, and then the partial large normal distribution function as a dynamic weighting function uation model, and thus the uation observations are sorted, with the final decisions)

Conjugate gradient method

双环并网逆变器matlab仿真,南京航天航空大学，自动控制系(double loop is fancy ,but there is more of than that control)

Example C-file S-function for defining a continuous system. * * x = Ax + Bu * y = Cx + Du * * For more details about S-functions, see simulink/src/sfuntmpl_doc.c.

The queueing example which is simplest for mathematical analysis is the M/M/1 queue. Here is the tcl script for it.

ل ك و د ب ي ف ر ق ب ي ن م ج م و ع ت ي ن م خ ت ل ف ي ن م ن ا ل ص و ر و ب ي ح ط ك ل و ا ح د ه ف ى ك ل ا س ف ا ك ر ة ا ل ك ل ا م د ه ؟ م ج م و ع ه ب ي ي د ي ه ا ا ص ف ا ر و م ج م و ع ه ب ي د ي ه ا و ح ا ي د

说明：  线性调频信号在雷达上的实现，文中给出了设计过程，具有很好的参考价值(LFM radar signals the realization of paper gives the design process, with a very good reference value)

一维移动最小二乘法以及最小二乘法的曲面拟合，可以直接使用(One dimensional moving least square method, which can be used directly)

3-D FDTD code of patch antenna in free space with Mur s boundary condition

说明：  分析并设计kalman滤波器，应用其对航天器得飞行状态量进行实时估计，得到较为准确的状态参量，(Kalman filter analysis and design, application of their spacecraft in real time the amount was estimated flight to get a more accurate state parameter,)