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motor_ClosedLoop
无刷直流电机转速电流双闭环仿真。逆变器、电机模型都是自建的,仿真精度较高。输出相电流为标准的方形波(The model is a speed-current dual-loop based simulation of BLDC. The inverter and the motor model are all built myself with high simulation accuracy. The output phase current of the motor is a standard square wave.)
- 2020-08-28 11:28:12下载
- 积分:1
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multicriculerlet-transform
multicirculerlet transform
- 2011-07-15 07:11:03下载
- 积分:1
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vsPmatlab
vs2010调用matlab.m文件生成的lib,dll,h文件,并进行参数的传递(vs2010 calling matlab.m files generated lib, dll, h file and pass parameters)
- 2013-11-27 21:42:54下载
- 积分:1
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HOGSVM
输入训练样本集和测试样本集,通过提取HOG然后用SVM实现分类。(Input training samples and test samples, extract HOG and implement classification with SVM.)
- 2018-04-26 09:07:43下载
- 积分:1
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test
这个程序主要编写了误码率和信道容量两个主程序和部分子程序(This program is mainly to write the bit error rate and channel capacity of two main program and part of the subroutine)
- 2012-05-10 16:37:37下载
- 积分:1
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2-Class
说明: 多类划分 matlab中使用数据挖掘的实例一个
方便新人参考(Matlab data mining multi-class classification)
- 2010-04-25 16:58:03下载
- 积分:1
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cc01
用Cohen--Coon整定公式来求P,PI,PID的个参数,其中Gc是校正器的传递函数,kp为比例系数, Ti为积分时间常数,Td为微分时间常数,输入参量vars为带迟滞--惯性环节模型的KT τ 输入参量vars为带迟滞--惯性环节的K T ι,已知参数k=vars(1);T=vars(2);ι=vars(3)。(With Cohen- Coon tuning formula to seek P, PI, PID' s parameters, which Gc is the corrector transfer function, kp the proportional coefficient, Ti the integral time constant, Td for the differential time constant, input parameters vars as with hysteresis- inertia model KT τ as input parameters vars with hysteresis- inertia of KT ι, the known parameters k = vars (1) T = vars (2) ι = vars (3).)
- 2010-05-18 20:37:26下载
- 积分:1
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IEEE14
IEEE14母线系统潮流计算的matlab程序(IEEE14 node flow calculation matlab program)
- 2012-07-04 11:18:35下载
- 积分:1
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optical-flow-lucas-kanade
descibes optical flow using lucas kanade algorithm. Example supplied help people understand easily
- 2013-07-24 13:05:05下载
- 积分:1
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proj1
MIT--航空航天工程中的计算方法_模拟飞机的动力学
MIT公开课程--航空航天工程中的计算方法
这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构,空气动力学,动力学和控制,和航空宇宙系统选出的。其技术包括:常微分方程系统的数值积分;偏微分方程式的有限差分,有限体积, 和有限元的离散化;数值线性代数;本征值问题和带有约束的最优化。(MIT- Aerospace Engineering in the calculation of simulated aircraft dynamics _ MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering calculations appear in an introduction. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization.)
- 2011-11-21 09:19:22下载
- 积分:1