MATLAB-Ch6DataAnalysis

无速度传感器的异步电机矢量控制书籍对学习电机的控制有很大的帮助(Speed ​ ​ sensorless induction motor vector control books of great help to learning motor control)

EKF+UKF滤波算法在汽车做二维运动中的应用(The EKF+ UKF filtering algorithm in two-dimensional movement in the car)

Packet-dropfunction functionfunction function

说明：  利用在box-muller 和在时域上通过低通滤波器的方法产生多普勒频移的瑞利信道(Using the box-muller, and in the time domain through a low pass filter method produces Doppler frequency shift of the Rayleigh channel)

计算冲击电压波下的Q-V图,雷电波或操作冲击波均可(simulation of q-v curv under thounder)

在图像处理时，有时需要用到图像分割。上述资料可以作为使用matlab进行图像分割的参考资料。(In the image processing, and sometimes need to use the image segmentation. The above information can be used as image segmentation using matlab reference.)

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)

用matlab语言编写的kalman滤波的demo 调试通过 滤波结果用图可直观看到 程序简单实用()

Optic communication antenna angle

对低密度校验矩阵的重建算法，LDPC应用在压缩感知中的一种算法(Low density parity check matrix of the reconstruction algorithm of LDPC applications in compression of the perception of an algorithm)