/usr/share/octave/packages/control-3.0.0/MDSSystem.m is in octave-control 3.0.0-5.
This file is owned by root:root, with mode 0o644.
The actual contents of the file can be viewed below.
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%% Robust control of a mass-damper-spring system.
%% Type @code{which MDSSystem} to locate,
%% @code{edit MDSSystem} to open and simply
%% @code{MDSSystem} to run the example file.
% ===============================================================================
% Robust Control of a Mass-Damper-Spring System Lukas Reichlin August 2011
% ===============================================================================
% Reference: Gu, D.W., Petkov, P.Hr. and Konstantinov, M.M.
% Robust Control Design with Matlab, Springer 2005
% ===============================================================================
% Tabula Rasa
clear all, close all, clc
% ===============================================================================
% System Model
% ===============================================================================
% +---------------+
% | d_m 0 0 |
% +-----| 0 d_c 0 |<----+
% u_m | | 0 0 d_k | | y_m
% u_c | +---------------+ | y_c
% u_k | | y_k
% | +---------------+ |
% +---->| |-----+
% | G_nom |
% u ----->| |-----> y
% +---------------+
% Nominal Values
m_nom = 3; % mass
c_nom = 1; % damping coefficient
k_nom = 2; % spring stiffness
% Perturbations
p_m = 0.4; % 40% uncertainty in the mass
p_c = 0.2; % 20% uncertainty in the damping coefficient
p_k = 0.3; % 30% uncertainty in the spring stiffness
% State-Space Representation
A = [ 0, 1
-k_nom/m_nom, -c_nom/m_nom ];
B1 = [ 0, 0, 0
-p_m, -p_c/m_nom, -p_k/m_nom ];
B2 = [ 0
1/m_nom ];
C1 = [ -k_nom/m_nom, -c_nom/m_nom
0, c_nom
k_nom, 0 ];
C2 = [ 1, 0 ];
D11 = [ -p_m, -p_c/m_nom, -p_k/m_nom
0, 0, 0
0, 0, 0 ];
D12 = [ 1/m_nom
0
0 ];
D21 = [ 0, 0, 0 ];
D22 = [ 0 ];
inname = {'u_m', 'u_c', 'u_k', 'u'}; % input names
outname = {'y_m', 'y_c', 'y_k', 'y'}; % output names
G_nom = ss (A, [B1, B2], [C1; C2], [D11, D12; D21, D22], ...
'inputname', inname, 'outputname', outname);
G = G_nom('y', 'u'); % extract output y and input u
% ===============================================================================
% Frequency Analysis of Uncertain System
% ===============================================================================
% Uncertainties: -1 <= delta_m, delta_c, delta_k <= 1
[delta_m, delta_c, delta_k] = ndgrid ([-1, 0, 1], [-1, 0, 1], [-1, 0, 1]);
% Bode Plots of Perturbed Plants
w = logspace (-1, 1, 100); % frequency vector
Delta = arrayfun (@(m, c, k) diag ([m, c, k]), delta_m(:), delta_c(:), delta_k(:), 'uniformoutput', false);
G_per = cellfun (@lft, Delta, {G_nom}, 'uniformoutput', false);
figure (1)
bode (G_per{:}, w)
legend off
% ===============================================================================
% Mixed Sensitivity H-infinity Controller Design (S over KS Method)
% ===============================================================================
% +-------+
% +--------------------->| W_p |----------> e_p
% | +-------+
% | +-------+
% | +---->| W_u |----------> e_u
% | | +-------+
% | | +---------+
% | | ->| |->
% r + e | +-------+ u | | G_nom |
% ----->(+)---+-->| K |----+--->| |----+----> y
% ^ - +-------+ +---------+ |
% | |
% +-----------------------------------------+
% Weighting Functions
s = tf ('s'); % transfer function variable
W_p = 0.95 * (s^2 + 1.8*s + 10) / (s^2 + 8.0*s + 0.01); % performance weighting
W_u = 10^-2; % control weighting
% Synthesis
K_mix = mixsyn (G, W_p, W_u); % mixed-sensitivity H-infinity synthesis
% Interconnections
L_mix = G * K_mix; % open loop
T_mix = feedback (L_mix); % closed loop
% ===============================================================================
% H-infinity Loop-Shaping Design (Normalized Coprime Factor Perturbations)
% ===============================================================================
% Settings
W1 = 8 * (2*s + 1) / (0.9*s); % precompensator
W2 = 1; % postcompensator
factor = 1.1; % suboptimal controller
% Synthesis
K_ncf = ncfsyn (G, W1, W2, factor); % positive feedback controller
% Interconnections
K_ncf = -K_ncf; % negative feedback controller
L_ncf = G * K_ncf; % open loop
T_ncf = feedback (L_ncf); % closed loop
% ===============================================================================
% Plot Results
% ===============================================================================
% Bode Plot
figure (2)
bode (K_mix, K_ncf)
% Step Response
figure (3)
step (T_mix, T_ncf, 10) % step response for 10 seconds
% ===============================================================================
|