fenleiqi

F16飞行控制仿真程序,针对F16战斗机做的飞行控制仿真(F16 flight control simulation program, to do for the F16 fighter flight control simulation)

实现用MATLAB程序产生歌曲，包括卡农，小星星和加勒比海盗的代码。(Songs MATLAB program, including Canon, little star, and Pirates of the Caribbean code.)

应用Oustaloup算法设计的滤波器理论，设计分数阶微分模块。用SIMULINK求解分数阶非线性微分方程(Application Oustaloup filter algorithm design theory, design, fractional differential module.Fractional Differential Equations with SIMULINK)

用局部参数最优化方法设计一个模型参考自适应系统,可调增益的初值Kc(0)=0.2，给定值r(t)为单位阶跃信号，即r(t)=A×1(t)。 要求： 1把连续系统离散化(采样时间可取0.1)。 2编制并运行这个系统的计算机程序(注意调整B值，使系统获得较好的自适应特性)。 3记录ym、yp的曲线 记录kp×kc的曲线 记录广义输出误差e的变化曲线。 4在参数收敛后，让Kp=2变为Kp=1，重新观察Kp×Kc及e的变化曲线。 5找出在确定的B值下，使系统不稳定的A值(阶跃信号的幅值)，并与用劳斯稳定判据计算的结果比较。 (With local parameter optimization method to design a model reference adaptive system, adjustable gain initial Kc (0) = 0.2, for a given value of r (t) for the unit step signal that r (t) = A × 1 ( t). Requirements: a continuous system discretization (sampling time of 0.1 preferred). 2 compiled and run the system computer program (Note B to adjust the value of the system to obtain better adaptive characteristics). 3 records ym, yp curve record kp × kc curve records generalized output error e curves. 4 parameter convergence, let Kp = 2 into the Kp = 1, re-observed Kp × Kc and e curves. B-5 to find value in determining the next, making the system unstable A value (step signal of amplitude), and using Routh stability criterion and the comparison of the results calculated.)

说明：  使用PSO解决参数识别问题,MATLAB源代码(Solve the parameter identification problem using the PSO, MATLAB source code )

solution of the integrals matlab

经过验证的基于奇排列的多相滤波matlab源代码(Validated based on polyphase filtering of the arrangement of the matlab source code)

Sorting and Searching Algorithms: A Cookbook

联邦滤波器三个通道滤波后数据融合结果，并考虑了丢包，能对高斯噪声及非线性滤波有较好的处理。(Federal filter three channel filtered data fusion results, taking into account the loss can Gaussian noise and nonlinear filtering process better.)

linedatas of IEEE standard systems for Optimal power flow