2018-10-12 18:17:03 +02:00
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function [axisc] = initializeAxisc()
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2018-06-16 22:57:54 +02:00
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%%
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axisc = struct();
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2018-10-12 13:22:29 +02:00
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axisc.m = 40; % [kg]
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2018-06-16 22:57:54 +02:00
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axisc.k.ax = 1; % TODO [N*m/deg)]
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2018-06-21 11:42:46 +02:00
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axisc.c.ax = (1/1)*sqrt(axisc.k.ax/axisc.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', 'axisc', '-append');
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2018-06-16 22:57:54 +02:00
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end
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