Add Compliance and Transmissibility computation
Change solid to rigid
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83
src/computeCompliance.m
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83
src/computeCompliance.m
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@@ -0,0 +1,83 @@
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function [C, C_norm, freqs] = computeCompliance(args)
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% computeCompliance -
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%
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% Syntax: [C, C_norm, freqs] = computeCompliance(args)
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%
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% Inputs:
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% - args - Structure with the following fields:
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% - plots [true/false] - Should plot the transmissilibty matrix and its Frobenius norm
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% - freqs [] - Frequency vector to estimate the Frobenius norm
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%
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% Outputs:
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% - C [6x6 ss] - Compliance matrix
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% - C_norm [length(freqs)x1] - Frobenius norm of the Compliance matrix
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% - freqs [length(freqs)x1] - Frequency vector in [Hz]
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arguments
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args.plots logical {mustBeNumericOrLogical} = false
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args.freqs double {mustBeNumeric, mustBeNonnegative} = logspace(1,4,1000)
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end
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freqs = args.freqs;
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%% Options for Linearized
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options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'stewart_platform_model';
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%% Input/Output definition
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clear io; io_i = 1;
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io(io_i) = linio([mdl, '/Disturbances/F_ext'], 1, 'openinput'); io_i = io_i + 1; % External forces [N, N*m]
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io(io_i) = linio([mdl, '/Absolute Motion Sensor'], 1, 'openoutput'); io_i = io_i + 1; % Absolute Motion [m, rad]
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%% Run the linearization
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C = linearize(mdl, io, options);
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C.InputName = {'Fdx', 'Fdy', 'Fdz', 'Mdx', 'Mdy', 'Mdz'};
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C.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'};
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p_handle = zeros(6*6,1);
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if args.plots
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fig = figure;
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for ix = 1:6
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for iy = 1:6
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p_handle((ix-1)*6 + iy) = subplot(6, 6, (ix-1)*6 + iy);
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hold on;
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plot(freqs, abs(squeeze(freqresp(C(ix, iy), freqs, 'Hz'))), 'k-');
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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if ix < 6
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xticklabels({});
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end
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if iy > 1
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yticklabels({});
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end
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end
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end
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linkaxes(p_handle, 'xy')
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xlim([freqs(1), freqs(end)]);
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han = axes(fig, 'visible', 'off');
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han.XLabel.Visible = 'on';
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han.YLabel.Visible = 'on';
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xlabel(han, 'Frequency [Hz]');
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ylabel(han, 'Compliance [m/N, rad/(N*m)]');
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end
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freqs = args.freqs;
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C_norm = zeros(length(freqs), 1);
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for i = 1:length(freqs)
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C_norm(i) = sqrt(trace(freqresp(C, freqs(i), 'Hz')*freqresp(C, freqs(i), 'Hz')'));
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end
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if args.plots
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figure;
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plot(freqs, C_norm)
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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xlabel('Frequency [Hz]');
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ylabel('Compliance - Frobenius Norm');
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end
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84
src/computeTransmissibility.m
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84
src/computeTransmissibility.m
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@@ -0,0 +1,84 @@
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function [T, T_norm, freqs] = computeTransmissibility(args)
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% computeTransmissibility -
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%
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% Syntax: [T, T_norm, freqs] = computeTransmissibility(args)
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%
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% Inputs:
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% - args - Structure with the following fields:
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% - plots [true/false] - Should plot the transmissilibty matrix and its Frobenius norm
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% - freqs [] - Frequency vector to estimate the Frobenius norm
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%
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% Outputs:
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% - T [6x6 ss] - Transmissibility matrix
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% - T_norm [length(freqs)x1] - Frobenius norm of the Transmissibility matrix
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% - freqs [length(freqs)x1] - Frequency vector in [Hz]
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arguments
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args.plots logical {mustBeNumericOrLogical} = false
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args.freqs double {mustBeNumeric, mustBeNonnegative} = logspace(1,4,1000)
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end
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freqs = args.freqs;
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%% Options for Linearized
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options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'stewart_platform_model';
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%% Input/Output definition
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clear io; io_i = 1;
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io(io_i) = linio([mdl, '/Disturbances/D_w'], 1, 'openinput'); io_i = io_i + 1; % Base Motion [m, rad]
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io(io_i) = linio([mdl, '/Absolute Motion Sensor'], 1, 'openoutput'); io_i = io_i + 1; % Absolute Motion [m, rad]
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%% Run the linearization
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T = linearize(mdl, io, options);
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T.InputName = {'Wdx', 'Wdy', 'Wdz', 'Wrx', 'Wry', 'Wrz'};
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T.OutputName = {'Edx', 'Edy', 'Edz', 'Erx', 'Ery', 'Erz'};
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p_handle = zeros(6*6,1);
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if args.plots
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fig = figure;
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for ix = 1:6
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for iy = 1:6
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p_handle((ix-1)*6 + iy) = subplot(6, 6, (ix-1)*6 + iy);
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hold on;
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plot(freqs, abs(squeeze(freqresp(T(ix, iy), freqs, 'Hz'))), 'k-');
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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if ix < 6
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xticklabels({});
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end
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if iy > 1
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yticklabels({});
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end
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end
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end
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linkaxes(p_handle, 'xy')
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xlim([freqs(1), freqs(end)]);
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ylim([1e-5, 1e2]);
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han = axes(fig, 'visible', 'off');
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han.XLabel.Visible = 'on';
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han.YLabel.Visible = 'on';
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ylabel(han, 'Frequency [Hz]');
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xlabel(han, 'Transmissibility [m/m]');
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end
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T_norm = zeros(length(freqs), 1);
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for i = 1:length(freqs)
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T_norm(i) = sqrt(trace(freqresp(T, freqs(i), 'Hz')*freqresp(T, freqs(i), 'Hz')'));
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end
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T_norm = T_norm/sqrt(6);
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if args.plots
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figure;
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plot(freqs, T_norm)
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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xlabel('Frequency [Hz]');
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ylabel('Transmissibility - Frobenius Norm');
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end
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@@ -6,17 +6,19 @@ function [ground] = initializeGround(args)
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% Inputs:
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% - args - Structure with the following fields:
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% - type - 'none', 'solid', 'flexible'
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% - rot_point [3x1] - Rotation point for the ground motion [m]
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% - K [3x1] - Translation Stiffness of the Ground [N/m]
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% - C [3x1] - Translation Damping of the Ground [N/(m/s)]
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%
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% Outputs:
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% - ground - Struture with the following properties:
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% - type - 1 (none), 2 (solid), 3 (flexible)
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% - type - 1 (none), 2 (rigid), 3 (flexible)
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% - K [3x1] - Translation Stiffness of the Ground [N/m]
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% - C [3x1] - Translation Damping of the Ground [N/(m/s)]
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arguments
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args.type char {mustBeMember(args.type,{'none', 'solid', 'flexible'})} = 'none'
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args.type char {mustBeMember(args.type,{'none', 'rigid', 'flexible'})} = 'none'
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args.rot_point (3,1) double {mustBeNumeric} = zeros(3,1)
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args.K (3,1) double {mustBeNumeric, mustBeNonnegative} = 1e8*ones(3,1)
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args.C (3,1) double {mustBeNumeric, mustBeNonnegative} = 1e1*ones(3,1)
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end
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@@ -24,7 +26,7 @@ end
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switch args.type
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case 'none'
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ground.type = 1;
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case 'solid'
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case 'rigid'
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ground.type = 2;
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case 'flexible'
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ground.type = 3;
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@@ -32,3 +34,5 @@ end
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ground.K = args.K;
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ground.C = args.C;
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ground.rot_point = args.rot_point;
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@@ -5,7 +5,7 @@ function [payload] = initializePayload(args)
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%
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% Inputs:
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% - args - Structure with the following fields:
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% - type - 'none', 'solid', 'flexible', 'cartesian'
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% - type - 'none', 'rigid', 'flexible', 'cartesian'
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% - h [1x1] - Height of the CoM of the payload w.r.t {M} [m]
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% This also the position where K and C are defined
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% - K [6x1] - Stiffness of the Payload [N/m, N/rad]
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@@ -15,7 +15,7 @@ function [payload] = initializePayload(args)
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%
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% Outputs:
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% - payload - Struture with the following properties:
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% - type - 1 (none), 2 (solid), 3 (flexible)
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% - type - 1 (none), 2 (rigid), 3 (flexible)
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% - h [1x1] - Height of the CoM of the payload w.r.t {M} [m]
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% - K [6x1] - Stiffness of the Payload [N/m, N/rad]
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% - C [6x1] - Stiffness of the Payload [N/(m/s), N/(rad/s)]
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@@ -23,7 +23,7 @@ function [payload] = initializePayload(args)
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% - I [3x3] - Inertia matrix for the Payload [kg*m2]
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arguments
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args.type char {mustBeMember(args.type,{'none', 'solid', 'flexible', 'cartesian'})} = 'none'
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args.type char {mustBeMember(args.type,{'none', 'rigid', 'flexible', 'cartesian'})} = 'none'
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args.K (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e8*ones(6,1)
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args.C (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e1*ones(6,1)
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args.h (1,1) double {mustBeNumeric, mustBeNonnegative} = 100e-3
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@@ -34,7 +34,7 @@ end
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switch args.type
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case 'none'
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payload.type = 1;
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case 'solid'
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case 'rigid'
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payload.type = 2;
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case 'flexible'
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payload.type = 3;
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