2018-10-12 13:22:29 +02:00
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function [ty] = initializeTy()
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2018-06-16 22:57:54 +02:00
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%%
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ty = struct();
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2018-10-12 13:22:29 +02:00
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ty.m = 250; % [kg]
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2018-06-16 22:57:54 +02:00
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ty.k.ax = 1e7/4; % Axial Stiffness for each of the 4 guidance (y) [N/m]
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ty.k.rad = 9e9/4; % Radial Stiffness for each of the 4 guidance (x-z) [N/m]
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2018-06-21 11:42:46 +02:00
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ty.c.ax = 100*(1/5)*sqrt(ty.k.ax/ty.m);
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ty.c.rad = 100*(1/5)*sqrt(ty.k.rad/ty.m);
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2018-06-16 22:57:54 +02:00
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2018-10-11 10:25:57 +02:00
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%% Save
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save('./mat/stages.mat', 'ty', '-append');
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2018-06-16 22:57:54 +02:00
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end
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