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simulink命令集(转载) 仿真命令: sim ---仿真运行一个simulink模块 sldebug ---调试一个simulink模块 simset ---设置仿真参数 simget ---获取仿真参数 线性化和整理命令: linmod ---从连续时间系统中获取线性模型(状态方程)-Simulink command sets (reproduced) simulation order : sim -- running a Simulink simulation module sldebug --- debug module simset a Simulink simulation parameters set --- --- access simget linear simulation parameters and collation order : from linmod --- continuous-time system access linear model (equation)
Update : 2008-10-13 Size : 4.08kb Publisher : 张焕焕


Update : 2025-02-19 Size : 4kb Publisher : 张焕焕

使用Linmod和dlinmod函数以提取线性模型-Use Linmod and dlinmod function to extract the linear model
Update : 2025-02-19 Size : 5kb Publisher : 孙新宇

使用Linmod和dlinmod函数以提取线性模型,
Update : 2025-02-19 Size : 5kb Publisher : 韩一广

1、利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型; 2、利用linmod对非线性模型线性化; 3、姿态模型线性化后,利用极点配置(pole)方法求取控制参数; 4、将控制参数带入非线性模型仿真控制效果。-One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude 2, the use of linmod linearization of the nonlinear model Attitude model linearization, the use of pole configuration (pole) is used to obtain the control parameters 4, the control parameters into the nonlinear model simulation control effect.
Update : 2025-02-19 Size : 9kb Publisher : 战斗机

根据一个质量弹簧系统建立系统的状态空间系统,并判断其能控性,并求系统的脉冲和阶跃响应曲线-According to a mass spring system to establish a system state space system, and its controllability, and system of pulse and step response curve
Update : 2025-02-19 Size : 21kb Publisher : 郑旭

MATLAB M-file m3.m is for the generator with series capacitor compensated case of Project 3 on subsynchronous resonance in Chapter 10. It is to be used with the SIMULINK files : s3.m and s3eig.m. The SIMULINK file s3eig.m is being used in conjunction with the trim and linmod functions of this script - MATLAB M-file m3.m is for the generator with series capacitor compensated case of Project 3 on subsynchronous resonance in Chapter 10. It is to be used with the SIMULINK files : s3.m and s3eig.m. The SIMULINK file s3eig.m is being used in conjunction with the trim and linmod functions of this script
Update : 2025-02-19 Size : 5kb Publisher : said

DL : 0
m3g.m is the MATLAB script file for the fixed terminal voltage case of Project 3 on synchronous resonance in Chapter 10. It is to be used with the SIMULINK files : s3g.m and s3geig.m. The SIMULINK file s3geig.m is referred to in the trim and linmod function calls of this script - m3g.m is the MATLAB script file for the fixed terminal voltage case of Project 3 on synchronous resonance in Chapter 10. It is to be used with the SIMULINK files : s3g.m and s3geig.m. The SIMULINK file s3geig.m is referred to in the trim and linmod function calls of this script
Update : 2025-02-19 Size : 4kb Publisher : vava

DL : 0
A linear model of the system can be extracted the Simulink model into the MATLAB workspace. This can accomplished employing the MATLAB command linmod or directly within Simulink as we will do here. We will specifically use the base Simulink model developed first principles shown below. You can download this model here, or you can refer to the DC Motor Speed: Simulink Modeling page to recreate the model yourself. -A linear model of the system can be extracted the Simulink model into the MATLAB workspace. This can accomplished employing the MATLAB command linmod or directly within Simulink as we will do here. We will specifically use the base Simulink model developed first principles shown below. You can download this model here, or you can refer to the DC Motor Speed: Simulink Modeling page to recreate the model yourself.
Update : 2025-02-19 Size : 8kb Publisher : pop pop

DL : 0
利用Matlabx线性化方法的得到的感应发电机风电机组模型-this code deals with obtaining a reduced-order linear model for a high-power induction-generator-based WECS by using the MATLAB® function linmod.
Update : 2025-02-19 Size : 8kb Publisher : LJH

航天器姿态控制仿真程序,利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型,利用linmod对非线性模型线性化。(The simulation program of spacecraft attitude control uses the sfunction method of Simulink to establish the dynamic model and kinematic model of spacecraft attitude, and uses limod to linearize the nonlinear model.)
Update : 2025-02-19 Size : 8kb Publisher : woyaokaobo
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