Fountain-Codes-Encoding-Algorithm

该程序适用于实现匹配滤波器的基于MATLAB编写(matchfilter)

用来解薛定谔方程的很好的代码，可以解氢原子及类似的原子的本征能谱(Solution of the Schrodinger equation for a good code, and similar solutions of hydrogen atoms in the intrinsic spectrum)

Image Reconstruction

复杂网络中的适应度模型，BA模型的改进，采用指数分布(To adapt to the complexity of the network model, BA model of improvement, the use of exponential distribution)

说明：  ESPRIT算法的性能与信噪比的关系，包括LS-ESPRIT算法,TLS-ESPRIT算法,TAM算法(ESPRIT algorithm performance and the relationship between SNR, including the LS-ESPRIT algorithm, TLS-ESPRIT algorithm, TAM algorithm)

电力电子、电机控制的仿真模型，异步电机无速度传感器控制(The simulation model of power electronics, motor control, induction motor speed sensorless control)

编制以M序列为输入时，脉冲响应的相关分析算法并检验。(The preparation of the M sequence as input, the impulse response of the correlation analysis algorithm and test.)

音频信号采集 根据二进制编码原则，实现音频信号的信息采集(AUODIO CATCH)

说明：  月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)

5扩32 扩频方法仿真 进行SNR估计 产生pn码 基带仿真(5 extended to 32 spread-spectrum method is estimated SNR simulation)