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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.)

有关gabor滤波 纹理特征提取 并且有很好的效果 可以试试(reference on gaborfiter and texture characteristics and works well)

常见信号的调制解调过程 如QPSK BPSK等(qpsk，bpsk and so on)

网络化控制系统的切换系统的非稳定性与稳定性的仿真分析(switched system stability)

说明：  内点优化法，stanford大学The Systems Optimization Laboratory 开发(Interior point,stanford university The Systems Optimization Laboratory)

Implementation of the canny edge detector.

理解快速傅里叶变换和反变换的好资料，是在MATLAB环境下联系的例子 (it is a good materials of understand the fast Fourier transform and inverse transform.)

关于ubuntu的各种学习资源，十分齐全(With regard to ubuntu a variety of learning resources, a very complete)

说明：  使用matlab gui编成的简易计算器，附带源码(easy calculate)

这里主要对LMS算法及一些改进的LMS算法（NLMS算法、变步长LMS算法、变换域LMS算法）之间的不同点进行了比较，在传统的LMS算法的基础上发展了LMS算法的应用。(here on the main LMS algorithm and some improvements to the LMS algorithm (NLMS. modified LMS algorithm, transform domain LMS algorithm) between the different points of comparison, in the traditional LMS algorithm developed on the basis of the LMS algorithm application.)