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echo on % This file demonstrates MATLAB's ability for classical control system % design by going through the design of a YAW DAMPER for a Jet Transport % aircraft. echo off % Copyright (c) 19

echo on clc echo off % Copyright (c) 1986-93 by the MathWorks, Inc. echo on % This demo shows the use of some of the control system design % and analysis tools available in MATLAB. % pause % S

% Embedded Control Systems in C/C++ % by Jim Ledin % % Chapter 3 linear models % This M-file requires the Control System Toolbox % Create a transfer function model tfplant = tf(100, [1 1.8 1

Embedded Control Systems in C/C++ by Jim Ledin Chapter 10 - Helicopter control system example This file describes the procedures for setup and operation of the 6DOF helicopter model and contro

% Embedded Control Systems in C/C++ % by Jim Ledin % % Chapter 10 - Helicopter control system example % % This M-file contains the linear models used in the % controller design for the Helicopte

% Embedded Control Systems in C/C++ % by Jim Ledin % % Chapter 10 - Helicopter control system example % % This M-file designs the controllers for the % Helicopter simulation % Set up the para

% Embedded Control Systems in C/C++ % by Jim Ledin % % Chapter 10 - Helicopter control system example % % This M-file sets up the system parameters for the % Helicopter simulation. % Units: M

Type=Exe Reference=*\G{00020430-0000-0000-C000-000000000046}#2.0#0#C:\WINNT\system32\stdole2.tlb#OLE Automation Reference=*\G{28E68F91-8D75-11D1-8DC3-3C302A000000}#1.0#0#C:\WINNT\system32\OPCDAAuto.

% Chapter 5: Figure 5.40, p. 273 % % Compute the response of the Mobile Robot Control % System to a triangular wave input. % numg=[10 20]; deng=[1 10 0]; [num,den]=cloop(numg,deng); t=[0:0.1:8.2

% Chapter 10: Figure 10.30, p. 608 % % Rotor winder control system transient response % for a simple gain controller with K=50, 100, 200, % and 300. % K=[50 100 200 500]; numg=[1]; deng=[1 15