代码搜索:Simulink 开发教程

找到约 10,000 项符合「Simulink 开发教程」的源代码

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txt matlab在弹道仿真中的应用.txt

分析了弹道仿真数学模型的特点、并以滑翔增程弹为例,详细研究了在M文 件、<mark>simulink</mark>工具箱以及两者交互使用环境下建立外弹道质心运动系统仿真模型的方法和优缺点。最后给出了一定条件下 的弹道仿真结果,以此证明该仿真算法对弹道进行仿真研究具有模型设计简单、参数易于修改和结果直观等特点。 ...
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cmm unix.cmm

# # unix.dsp # Template makefile for building a UNIX-based stand-alone # nonreal-time version of SIMULINK model using generated C code. # # Edited for use with DSP Blockset, v1.0. # # This make
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m trim_fun.m

%===================================================== % F16 nonlinear model trim cost function % for longitudinal motion, steady level flight % (cost = sum of weighted squared state derivat
www.eeworm.com/read/408813/11369184

m trim_fun.m

%===================================================== % F16 nonlinear model trim cost function % for longitudinal motion, steady level flight % (cost = sum of weighted squared state derivat
www.eeworm.com/read/338523/12300981

h ex38s2_acc.h

/* * ex38s2_acc.h * * Real-Time Workshop code generation for Simulink model "ex38s2_acc.mdl". * * Model Version : 1.58 * Real-Time Workshop file version : 4.0 $
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h ex38s1_acc.h

/* * ex38s1_acc.h * * Real-Time Workshop code generation for Simulink model "ex38s1_acc.mdl". * * Model Version : 1.55 * Real-Time Workshop file version : 4.0 $
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cmm unix.cmm

# # unix.dsp # Template makefile for building a UNIX-based stand-alone # nonreal-time version of SIMULINK model using generated C code. # # Edited for use with DSP Blockset, v1.0. # # This make
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m trim_fun.m

%===================================================== % F16 nonlinear model trim cost function % for longitudinal motion, steady level flight % (cost = sum of weighted squared state derivat
www.eeworm.com/read/367555/9742589

m trim_fun.m

%===================================================== % F16 nonlinear model trim cost function % for longitudinal motion, steady level flight % (cost = sum of weighted squared state derivat
www.eeworm.com/read/411673/11234004

m trim_fun.m

%===================================================== % F16 nonlinear model trim cost function % for longitudinal motion, steady level flight % (cost = sum of weighted squared state derivat