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PID_MATLAB
非常全面的控制系统PID仿真源码，适用控制类行业，先进PID控制及其MATLAB仿真_第二版(A very comprehensive simulation of PID control system source code, application control class industry)
- 2009-09-27 21:29:30下载
- 积分：1
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LS
说明： Mathematical models- choice of model class LS
- 2010-04-24 00:06:34下载
- 积分：1
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HIGH-OPTICS-SIMULATION
high optics simulation
- 2014-08-15 06:05:52下载
- 积分：1
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Gauss_Seidel
一种非线性代数方程组的迭代解法。最早用于解算电力系统潮流。这种方法具有程序编制简单、占用内存少的优点，但算法收敛性差，计算时间长。(In numerical linear algebra, the Gauss–Seidel method, also known as the Liebmann method or the method of successive displacement, is an iterative method used to solve a linear system of equations. It is named after the German mathematicians Carl Friedrich Gauss and Philipp Ludwig von Seidel, and is similar to the Jacobi method. Though it can be applied to any matrix with non-zero elements on the diagonals, convergence is only guaranteed if the matrix is either diagonally dominant, or symmetric and positive definite. It was only mentioned in a private letter Gauss to his student Gerling in 1823.[1] A publication was not delivered before 1874 by Seidel.)
- 2014-11-20 22:12:52下载
- 积分：1
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second_order_systems
This submission contains 3 examples to illustrate the change in peak time, settling time and percent overshoot as the poles of a 2nd order system move horizontaly,
- 2015-02-03 16:33:33下载
- 积分：1
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aco
蚁群算法ACO的应用，包括图像匹配，边缘检测，点检测，以及遗传算法GA(ACO ACO algorithm applications, including image matching, edge detection, detection, and genetic algorithm GA)
- 2014-05-20 21:25:21下载
- 积分：1
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PCB_FDTD
Pcb programing in matlab
- 2010-10-19 00:43:50下载
- 积分：1
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Myprog
说明： 电力能源预测，一个很好的模拟程序，可以供参考(electrical energy projections, a very good simulation program, to be available for reference)
- 2006-04-28 22:41:30下载
- 积分：1
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yuv-attack
该MATLAB代码可以实现一般的YUV攻击测试。(The MATLAB code can achieve a general YUV attack test.)
- 2013-04-01 18:00:43下载
- 积分：1
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han1
这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)
- 2020-11-03 20:39:53下载
- 积分：1
