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解线性方程组的一种迭代法，类似于共轭斜量法：预善共轭斜量法(Solution of linear equations of a iterative method, similar to conjugate oblique method: Pre-good conjugate oblique method)

说明：  matlab教程，以ppt的形式，比较简单、实例很充分. 初学者可以看看。(matlab tutorial to ppt the form of relatively simple, very good examples. beginner can look at.)

fisher分类器matlab代码，只具有二分类特性，可运行(fisher classifier matlab code, has only two classification features, you can run)

sampling programs in matlab

用MATLAB写的ekfukf工具包。绝对高质量代码。很方便拓展。在控制，估计领域应用广泛！(Written ekfukf using MATLAB tool kit. Absolute quality code. Easy to expand. )

Phased array antenna pattern (Chebyshev weights), In matlab R2009b debugging through, Algorithm for researchers to do reference.

Near to Far field transformation for antenna pattern

高斯消去法，用Matlab实现的。显然没有matlab自带的算法好，所以是练习以及和其他算法比较用的。(Gaussian elimination method, implemented with Matlab. Obviously there is no algorithm matlab own good, so is the practice and compare with other algorithms used.)

MATLAB GUI设计学习手记(第2版)(MATLAB GUI Design Learning Notes (2nd Edition))

编程仿真连续小推力实现GTO到GEO的三阶段转移过程，其中推力器的推力大小为0.8N，轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度，近地点角距为90度。 GTO轨道： ph:185km，ah：35786km，i：28.5°，GEO轨道：h：35786km，i：0°。 卫星质量为6600kg，从GTO到GEO，采用5000s的推力器。取地球半径为6378km，g取值为9.8m/s^2(The three stage transfer process from GTO to GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN is 0 degrees, 90 degrees for the argument of perigee. GTO orbit: ph:185km, ah:35786km, i:28.5, GEO orbit: h:35786km, i:0. The mass of the satellite is 6600kg, from GTO to GEO, using the 5000S thruster. The radius of the earth is 6378km, and the value of G is 9.8m/s^2)