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Rafal_Majorczyk_Sharp8_AssignmentA
Goal of the project was to implement numerical methods for solving systems of linear algebraic equations using MATLAB software. First of all I had to learn the structures of programming in MATLAB, later on I was able to implement and test numerical algorithms for solving given problems. All results, comments and conclusion are placed in this report. At the end of the report one can find my MATLAB programs, and sources which were used as a help for me during evaluation. Each task is presented under separated heading, with its full description, problem discussion, my approach for solving it and explanation.
- 2011-05-11 20:56:58下载
- 积分:1
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LMS
自适应滤波算法的实现,包括LMS算法与RLS算法。能够实现自适应滤波。(Adaptive filtering algorithm, including the LMS algorithm and RLS algorithm. Adaptive filtering can be achieved.)
- 2020-06-29 23:00:01下载
- 积分:1
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笼型异步交流风机
说明: 笼型异步发电机组模型,包括风力机,发电机等,可运行(Detailed model and grid-connected control of doubly-fed fan can be operated.)
- 2019-07-10 23:13:03下载
- 积分:1
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Matlab
matlab 蚁群算法算法 matlab代码(matlab matlab code ant colony algorithm)
- 2010-07-25 15:05:23下载
- 积分:1
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BBOSPEA2_Demo
说明: BBO进化算法-基于生物地理学新型进化算法(BBO evolutionary algorithm- a new evolutionary algorithm based on biogeography)
- 2011-03-01 19:34:34下载
- 积分:1
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script_ber_mimo_mmse_sic_bpsk_rayleigh_channel
computing the BER for BPSK modulation Cancellation (ZF-SIC) with optimal ordering
- 2011-03-29 21:42:28下载
- 积分:1
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LSSVM3DNL
10*10*10最小二乘支持向量机三维节点定位算法matlab源程序(10* 10* 10 squares support vector machine three-dimensional localization algorithms in Matlab source)
- 2020-10-05 10:27:38下载
- 积分:1
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rwimages
for read and write multiple image
- 2014-11-08 14:47:28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
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muller
求解图像的穆勒矩阵及其极分解矩阵,还有矩阵分析参数(Muller matrix and polar factorization matrix for solving image)
- 2017-07-02 10:01:33下载
- 积分:1