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desribes how to connect pscad through matlab

跳频通信系统 抗干扰分析 基于matlab(Anti-interference analysis, frequency hopping communication system)

Tactial+and+Strategic+Missile+Guidance一书第五版 Matlab格式程序代码(Tactial+and+Strategic+Missile+Guidance book fifth edition of the the Matlab format of the program code)

说明：  matlab实现：①递推增广最小二乘参数估计（RELS）②确定性系统的递推梯度校正参数估计（RGC）③递推最小二乘参数估计（RLS）④递推极大似然参数估计（RML）⑤递推随机牛顿参数估计（RSNA）(Matlab: (1) augmented recursive least square parameters estimation (RELS) (2) of a deterministic system recursive gradient correction parameter estimation (RGC) (3) recursive least squares (RLS) (4) parameter estimation, the recursive maximum likelihood parameter estimation (RML) (5) recursive random Newton parameter estimation (RSNA) )

数字波束形成，更改指向，更改阵元数量，加噪声(DBF beam forming )

产生雷达一维距离像，雷达视线角度连续变换的一系列一维距离像(A radar one-dimensional range radar line-of-sight angle continuous transformation of a series of one-dimensional range profile)

papers based on distributed arithmetic.

说明：  月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)

粒子群算法，基于粒子群算法的简单程序，主要是粒子群算法(Particle Swarm Optimizer)

基于MATLABD的线性二次型最优控制设计.二次型最优控制设计(MATLABD based on the linear quadratic optimal control design. Quadratic Optimal Control Design)