资源列表
uavsimul
- 开发无人飞行器采用的simulink仿真程序，能够实现姿态控制和避障-uav simulink model
Sliding-Mode-Robust-Control
- 基于趋近律的滑模鲁棒控制，实现了对二阶系统的滑模控制，并很好的实现了轨迹跟踪-Based reaching law sliding mode robust control, to achieve the second-mode control, and to achieve a good tracking
fdqcl
- solving rate equation of quantum cascade laser
FEM
- 利用有限元方法求解悬臂梁的振动问题,输入节点数可以算出前六阶振型，计算固有频率-Using the finite element method to solve the vibration problem of a cantilever beam, the input nodes can calculate the first six vibration mode, calculate the natural frequency
Missile-Spiral-trajectory
- 反导导弹末制导与控制论文及导弹螺旋弹道生成文件，可正确运行。-At the end of the anti-missile missiles and missile guidance and control paper spiral trajectory generated files, you can run correctly.
Application_Platform_CRS_V1.0
- 电控柴油系统标定平台，本平台实现了对INCA的调用和标定模块的添加和修改，以及集成了标定辅助工具-Electronically controlled Diesel system calibration platform, this platform to add and modify to INCA call and calibration modules, and integrated calibration aids
read_comtrade
- 解析Comtrade数据文件 电力行业标准数据文件-decode the Comtrade file
Schrodinger_Poisson_MQW
- shrodinger-poisson multi quantum well matlab simulatio file
AR
- AR法模拟脉动风场风速，matlab程序-AR methods，for fluctuate wind simulation
ACO-OFDM 代码
- aco-OFDM optical , design in matlab 代码
DVHop
- 基于DV-Hop的定位算法，利用三边测量以及极大似然估计法实现定位，误差较低，有误差分析图。-Based on DV-Hop localization algorithm, using trilateration and maximum likelihood estimation method to achieve localization, lower error margin of error analysis chart.
FFT
- 1.x=0.5*sin(2*pi*15*t)+2*sin(2*pi*40*t)。采样频率fs=100Hz，分别绘制N=128、1024点幅频图。 2.x=0.5*sin(2*pi*15*t)+2*sin(2*pi*40*t),fs=100Hz,绘制： （1）数据个数N=32，FFT所用的采样点数NFFT=32； （2）N=32，NFFT=128； （3）N=136，NFFT=128； （4）N=136，NFFT=512。-1. X = 0.5* sin (2* PI* 15*