Axis Compensator has been added
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@ -238,6 +238,9 @@ initializeRz();
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%% Initialize Hexapod Symétrie
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%% Initialize Hexapod Symétrie
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initializeMicroHexapod();
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initializeMicroHexapod();
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%% Initialize Center of gravity compensation
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initializeAxisc();
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#+end_src
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#+end_src
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** Center of Mass of each solid body
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** Center of Mass of each solid body
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@ -381,15 +384,16 @@ initializeMicroHexapod();
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end
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end
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#+end_src
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#+end_src
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** Bis
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For Granite Fx to Tx/Ty/Tz/Rx/Ry/Rz
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For Granite Fx to Tx/Ty/Tz/Rx/Ry/Rz
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#+begin_src matlab
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#+begin_src matlab
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dirs = {'x', 'y', 'z', 'rx', 'ry', 'rz'};
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dirs = {'x', 'y', 'z', 'rx', 'ry', 'rz'};
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stages = {'gtop', 'ty', 'ry', 'rz', 'hexa'}
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stages = {'gtop', 'ty', 'ry', 'rz', 'hexa'}
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n_stg = 2;
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n_stg = 5;
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n_exc = 2;
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n_exc = 3;
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f = logspace(1, 3, 1000);
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f = logspace(0, 3, 1000);
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figure;
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figure;
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for n_dir = 1:6
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for n_dir = 1:6
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@ -1070,6 +1070,16 @@ This Matlab function is accessible [[file:../src/initializeGranite.m][here]].
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#+begin_src matlab
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#+begin_src matlab
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function [granite] = initializeGranite()
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function [granite] = initializeGranite()
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%% Default values for opts
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opts = struct('rigid', false);
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%% Populate opts with input parameters
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if exist('opts_param','var')
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for opt = fieldnames(opts_param)'
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opts.(opt{1}) = opts_param.(opt{1});
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end
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end
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%%
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%%
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granite = struct();
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granite = struct();
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@ -1083,22 +1093,27 @@ This Matlab function is accessible [[file:../src/initializeGranite.m][here]].
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granite.mass_top = 4000; % [kg] TODO
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granite.mass_top = 4000; % [kg] TODO
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%% Dynamical Properties
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%% Dynamical Properties
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if opts.rigid
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granite.k.x = 1e12; % [N/m]
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granite.k.y = 1e12; % [N/m]
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granite.k.z = 1e12; % [N/m]
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granite.k.rx = 1e10; % [N*m/deg]
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granite.k.ry = 1e10; % [N*m/deg]
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granite.k.rz = 1e10; % [N*m/deg]
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else
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granite.k.x = 4e9; % [N/m]
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granite.k.x = 4e9; % [N/m]
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granite.c.x = 0.1*sqrt(granite.mass_top*granite.k.x); % [N/(m/s)]
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granite.k.y = 3e8; % [N/m]
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granite.k.y = 3e8; % [N/m]
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granite.c.y = 0.1*sqrt(granite.mass_top*granite.k.y); % [N/(m/s)]
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granite.k.z = 8e8; % [N/m]
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granite.k.z = 8e8; % [N/m]
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granite.c.z = 0.5*sqrt(granite.mass_top*granite.k.z); % [N/(m/s)]
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granite.k.rx = 1e4; % [N*m/deg]
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granite.k.rx = 1e4; % [N*m/deg]
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granite.c.rx = 0.1*sqrt(granite.mass_top*granite.k.rx); % [N*m/(deg/s)]
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granite.k.ry = 1e4; % [N*m/deg]
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granite.k.ry = 1e4; % [N*m/deg]
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granite.c.ry = 0.1*sqrt(granite.mass_top*granite.k.ry); % [N*m/(deg/s)]
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granite.k.rz = 1e6; % [N*m/deg]
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granite.k.rz = 1e6; % [N*m/deg]
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end
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granite.c.x = 0.1*sqrt(granite.mass_top*granite.k.x); % [N/(m/s)]
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granite.c.y = 0.1*sqrt(granite.mass_top*granite.k.y); % [N/(m/s)]
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granite.c.z = 0.5*sqrt(granite.mass_top*granite.k.z); % [N/(m/s)]
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granite.c.rx = 0.1*sqrt(granite.mass_top*granite.k.rx); % [N*m/(deg/s)]
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granite.c.ry = 0.1*sqrt(granite.mass_top*granite.k.ry); % [N*m/(deg/s)]
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granite.c.rz = 0.1*sqrt(granite.mass_top*granite.k.rz); % [N*m/(deg/s)]
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granite.c.rz = 0.1*sqrt(granite.mass_top*granite.k.rz); % [N*m/(deg/s)]
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%% Positioning parameters
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%% Positioning parameters
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@ -1176,11 +1191,12 @@ This Matlab function is accessible [[file:../src/initializeTy.m][here]].
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%% Y-Translation - Dynamicals Properties
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%% Y-Translation - Dynamicals Properties
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if opts.rigid
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if opts.rigid
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ty.k.ax = 1e10; % Axial Stiffness for each of the 4 guidance (y) [N/m]
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ty.k.ax = 1e12; % Axial Stiffness for each of the 4 guidance (y) [N/m]
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ty.k.rad = 1e12; % Radial Stiffness for each of the 4 guidance (x-z) [N/m]
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else
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else
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ty.k.ax = 1e7; % Axial Stiffness for each of the 4 guidance (y) [N/m]
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ty.k.ax = 5e7; % Axial Stiffness for each of the 4 guidance (y) [N/m]
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ty.k.rad = 5e7; % Radial Stiffness for each of the 4 guidance (x-z) [N/m]
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end
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end
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ty.k.rad = 1e8; % Radial Stiffness for each of the 4 guidance (x-z) [N/m]
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ty.c.ax = 0.1*sqrt(ty.k.ax*ty.m);
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ty.c.ax = 0.1*sqrt(ty.k.ax*ty.m);
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ty.c.rad = 0.1*sqrt(ty.k.rad*ty.m);
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ty.c.rad = 0.1*sqrt(ty.k.rad*ty.m);
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@ -1238,14 +1254,16 @@ This Matlab function is accessible [[file:../src/initializeRy.m][here]].
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%% Tilt Stage - Dynamical Properties
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%% Tilt Stage - Dynamical Properties
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if opts.rigid
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if opts.rigid
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ry.k.tilt = 1e10; % Rotation stiffness around y [N*m/deg]
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ry.k.tilt = 1e10; % Rotation stiffness around y [N*m/deg]
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ry.k.h = 1e12; % Stiffness in the direction of the guidance [N/m]
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ry.k.rad = 1e12; % Stiffness in the top direction [N/m]
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ry.k.rrad = 1e12; % Stiffness in the side direction [N/m]
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else
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else
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ry.k.tilt = 1e3; % Rotation stiffness around y [N*m/deg]
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ry.k.tilt = 1e4; % Rotation stiffness around y [N*m/deg]
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ry.k.h = 1e8; % Stiffness in the direction of the guidance [N/m]
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ry.k.rad = 1e8; % Stiffness in the top direction [N/m]
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ry.k.rrad = 1e8; % Stiffness in the side direction [N/m]
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end
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end
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ry.k.h = 357e6/4; % Stiffness in the direction of the guidance [N/m]
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ry.k.rad = 555e6/4; % Stiffness in the top direction [N/m]
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ry.k.rrad = 238e6/4; % Stiffness in the side direction [N/m]
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ry.c.h = 0.1*sqrt(ry.k.h*ry.m);
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ry.c.h = 0.1*sqrt(ry.k.h*ry.m);
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ry.c.rad = 0.1*sqrt(ry.k.rad*ry.m);
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ry.c.rad = 0.1*sqrt(ry.k.rad*ry.m);
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ry.c.rrad = 0.1*sqrt(ry.k.rrad*ry.m);
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ry.c.rrad = 0.1*sqrt(ry.k.rrad*ry.m);
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@ -1302,15 +1320,17 @@ This Matlab function is accessible [[file:../src/initializeRz.m][here]].
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rz.m = 250; % [kg]
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rz.m = 250; % [kg]
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%% Spindle - Dynamical Properties
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%% Spindle - Dynamical Properties
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% Estimated stiffnesses
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rz.k.ax = 2e9; % Axial Stiffness [N/m]
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rz.k.rad = 7e8; % Radial Stiffness [N/m]
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rz.k.tilt = 1e8*(2*pi/360); % Rotational Stiffness [N*m/deg]
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if opts.rigid
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if opts.rigid
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rz.k.rot = 1e10; % Rotational Stiffness [N*m/deg]
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rz.k.rot = 1e10; % Rotational Stiffness (Rz) [N*m/deg]
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rz.k.tilt = 1e10; % Rotational Stiffness (Rx, Ry) [N*m/deg]
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rz.k.ax = 1e12; % Axial Stiffness (Z) [N/m]
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rz.k.rad = 1e12; % Radial Stiffness (X, Y) [N/m]
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else
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else
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rz.k.rot = 1e6; % TODO what value should I put? [N*m/deg]
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rz.k.rot = 1e6; % TODO - Rotational Stiffness (Rz) [N*m/deg]
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rz.k.tilt = 1e6; % Rotational Stiffness (Rx, Ry) [N*m/deg]
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rz.k.ax = 2e9; % Axial Stiffness (Z) [N/m]
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rz.k.rad = 7e8; % Radial Stiffness (X, Y) [N/m]
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end
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end
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% Damping
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% Damping
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@ -1337,7 +1357,7 @@ This Matlab function is accessible [[file:../src/initializeMicroHexapod.m][here]
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#+begin_src matlab
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#+begin_src matlab
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function [micro_hexapod] = initializeMicroHexapod(opts_param)
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function [micro_hexapod] = initializeMicroHexapod(opts_param)
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%% Default values for opts
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%% Default values for opts
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opts = struct();
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opts = struct('rigid', false);
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%% Populate opts with input parameters
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%% Populate opts with input parameters
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if exist('opts_param','var')
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if exist('opts_param','var')
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@ -1380,7 +1400,7 @@ This Matlab function is accessible [[file:../src/initializeMicroHexapod.m][here]
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Leg.stroke = 10e-3; % Maximum Stroke of each leg [m]
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Leg.stroke = 10e-3; % Maximum Stroke of each leg [m]
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Leg.k.ax = 5e7; % Stiffness of each leg [N/m]
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Leg.k.ax = 5e7; % Stiffness of each leg [N/m]
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Leg.ksi.ax = 3; % Maximum amplification at resonance []
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Leg.ksi.ax = 0.1; % Modal damping ksi = 1/2*c/sqrt(km) []
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Leg.rad.bottom = 25; % Radius of the cylinder of the bottom part [mm]
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Leg.rad.bottom = 25; % Radius of the cylinder of the bottom part [mm]
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Leg.rad.top = 17; % Radius of the cylinder of the top part [mm]
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Leg.rad.top = 17; % Radius of the cylinder of the top part [mm]
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Leg.density = 8000; % Density of the material [kg/m^3]
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Leg.density = 8000; % Density of the material [kg/m^3]
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@ -1433,7 +1453,7 @@ This Matlab function is accessible [[file:../src/initializeMicroHexapod.m][here]
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function [element] = updateDamping(element)
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function [element] = updateDamping(element)
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field = fieldnames(element.k);
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field = fieldnames(element.k);
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for i = 1:length(field)
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for i = 1:length(field)
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element.c.(field{i}) = 1/element.ksi.(field{i})*sqrt(element.k.(field{i})/element.m);
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element.c.(field{i}) = 2*element.ksi.(field{i})*sqrt(element.k.(field{i})*element.m);
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end
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end
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end
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end
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