qira_peg

蒙特卡洛模拟的例子以及程序 关于结构可靠度分析的 有需要的可以下载看看(Examples and programs of Monte Carlo simulation)

说明：  一种在代数结构中的常用算法，对于伽罗华域的各种计算，非常适合各种编码算法(Algebraic structure of a common algorithm, for a variety of computing Galois field, ideal for a variety of coding algorithms)

说明：  matlab系统仿真实例，m10_1.rar，适合MATLAB初学(matlab simulation examples, m10_1.rar, suitable for beginners MATLAB)

The Prediction Algorithm Based on Fuzzy Logic(Gradient_Descent approach)

simulation of BER of a MIMO system using STBC

说明：  Jacobi的matlab程序是我同学编着玩的，我试了一下挺好，Jacobi迭代算法。(Jacobi s matlab program is edited by students, I play, I tried some very good, Jacobi iterative algorithm.)

（一）目的：通过对常用的概率密度函数和分布函数的应用，达到熟练掌握概率密度函数和分布函数调用方法的目的。 （二）任务：对实际的案例进行分析，调用相应概率密度函数和分布函数，使用MATLAB软件计算其结果。 （三）要求：理解概率密度函数和分布函数，能够解决实际问题。 ((A) Purpose: used by the probability density function and distribution function of the application, to master the probability density function and distribution methods of the purpose of function call. (B) tasks: the actual analysis of the case, call the corresponding probability density function and distribution function, the use of MATLAB software to calculate their results. (C) requirements: understanding of the probability density function and distribution function, to solve practical problems.)

雷达数据处理中文经典教材，系统地介绍了国内外多年来雷达数据自理技术的研究进展情况及作者们的研究成果，对雷达系统设计学习者有较大帮助。(Chinese classic radar data processing materials, a systematic introduction to radar data at home and abroad for many years the progress of self-care technology research and the authors of the research results, the radar system design learners have more help.)

使用矩量法计传输线上的驻波，并将结果显示出来．(The use of moment method of transmission lines of the standing wave, and the results are displayed.)

这个课题设计从地球的近地轨道起飞到达谷神星预定轨道并且着陆在其表面上的一种数值方法。基于有限时间的航行纠正点火而非瞬时推力数值计算和Matlab仿真。最后可以看到空间飞行器从地球的影响球飞到谷神星的影响球的飞行轨迹。(This project explores the mathematical methods and results of designing a mission to land a spacecraft on the asteroid Ceres by beginning in an earth-centered LEO orbit and ending in an orbit prepared to land on the surface of the asteroid. Rather than assume instantaneous velocity changes, course-correcting burns of finite time are considered and analyzed using numerical methods and Matlab computation. The behavior of the spacecraft is observed inside the Earth s sphere of influence, in interplanetary space, and inside Ceres sphere of influence. )