[major-changes] use of referenced model, use of variable step solver
This commit is contained in:
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5e6f1dbc38
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@ -1,75 +0,0 @@
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%% Load open loop data
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% gm_ol = load('../data/ground_motion_001.mat');
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%%
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clear; close all; clc;
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%%
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sim Assemblage;
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%%
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Dsample.Data = Dsample.Data - Dsample.Data(1, :);
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%% Time domain X-Y-Z
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figure;
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hold on;
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plot(Dsample.Time, Dsample.Data(:, 1));
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plot(Dsample.Time, Dsample.Data(:, 2));
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plot(Dsample.Time, Dsample.Data(:, 3));
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legend({'x', 'y', 'z'})
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hold off;
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xlabel('Time [s]'); ylabel('Displacement [m]');
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exportFig('tomo_time_translations', 'normal-normal')
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%% Time domain angles
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figure;
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hold on;
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plot(Dsample.Time, Dsample.Data(:, 4));
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plot(Dsample.Time, Dsample.Data(:, 5));
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plot(Dsample.Time, Dsample.Data(:, 6));
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legend({'$\theta_x$', '$\theta_y$', '$\theta_z$'})
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hold off;
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xlabel('Time [s]'); ylabel('Angle [rad]');
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exportFig('tomo_time_rotations', 'normal-normal')
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%% PSD X-Y-Z
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han_windows = hanning(ceil(length(Dsample.Time)/10));
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[psd_x, freqs_x] = pwelch(Dsample.Data(:, 1), han_windows, 0, [], 1/Ts);
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[psd_y, freqs_y] = pwelch(Dsample.Data(:, 2), han_windows, 0, [], 1/Ts);
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[psd_z, freqs_z] = pwelch(Dsample.Data(:, 3), han_windows, 0, [], 1/Ts);
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figure;
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hold on;
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plot(freqs_x, sqrt(psd_x));
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plot(freqs_y, sqrt(psd_y));
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plot(freqs_z, sqrt(psd_z));
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set(gca,'xscale','log'); set(gca,'yscale','log');
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xlabel('Frequency [Hz]'); ylabel('PSD [$m/\sqrt{Hz}$]');
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legend({'x', 'y', 'z'})
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hold off;
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exportFig('tomo_psd_translations', 'normal-normal')
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%% PSD
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han_windows = hanning(ceil(length(Dsample.Time)/10));
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[psd_x, freqs_x] = pwelch(Dsample.Data(:, 4), han_windows, 0, [], 1/Ts);
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[psd_y, freqs_y] = pwelch(Dsample.Data(:, 5), han_windows, 0, [], 1/Ts);
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[psd_z, freqs_z] = pwelch(Dsample.Data(:, 6), han_windows, 0, [], 1/Ts);
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figure;
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hold on;
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plot(freqs_x, sqrt(psd_x));
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plot(freqs_y, sqrt(psd_y));
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plot(freqs_z, sqrt(psd_z));
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set(gca,'xscale','log'); set(gca,'yscale','log');
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xlabel('Frequency [Hz]'); ylabel('PSD [$rad/s/\sqrt{Hz}$]');
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legend({'$\theta_x$', '$\theta_y$', '$\theta_z$'})
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hold off;
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exportFig('tomo_psd_rotations', 'normal-normal')
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%%
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save('./data/ground_motion.mat', 'Dsample')
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BIN
Assemblage.slx
BIN
Assemblage.slx
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@ -2,4 +2,4 @@
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clear; close all; clc;
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%%
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sim('Micro_Station_Displacement.slx');
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sim('sim_nano_station_disp.slx');
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@ -3,7 +3,7 @@ clear; close all; clc;
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%% Initialize simulation configuration
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opts_sim = struct(...
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'Tsim', 1 ...
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'Tsim', 0.1 ...
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);
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initializeSimConf(opts_sim);
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@ -14,36 +14,33 @@ load('./mat/sim_conf.mat', 'sim_conf')
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time_vector = 0:sim_conf.Ts:sim_conf.Tsim;
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% Translation Stage
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ty = 0*ones(length(time_vector), 1);
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Ty = 0.20*ones(length(time_vector), 1);
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% Tilt Stage
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ry = 2*pi*(0/360)*ones(length(time_vector), 1);
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% ry = 2*pi*(3/360)*sin(2*pi*time_vector);
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Ry = 2*pi*(3/360)*ones(length(time_vector), 1);
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% Ry = 2*pi*(3/360)*sin(2*pi*time_vector);
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% Spindle
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rz = 2*pi*1*(time_vector);
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% rz = 2*pi*(190/360)*ones(length(time_vector), 1);
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Rz = 2*pi*3*(time_vector);
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% Rz = 2*pi*(190/360)*ones(length(time_vector), 1);
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% Micro Hexapod
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u_hexa = zeros(length(time_vector), 6);
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Dh = zeros(length(time_vector), 6);
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% Gravity Compensator system
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mass = zeros(length(time_vector), 2);
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mass(:, 2) = pi;
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Dm = zeros(length(time_vector), 2);
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Dm(:, 2) = pi;
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opts_inputs = struct(...
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'ty', ty, ...
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'ry', ry, ...
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'rz', rz, ...
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'u_hexa', u_hexa, ...
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'mass', mass ...
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'Ty', Ty, ...
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'Ry', Ry, ...
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'Rz', Rz, ...
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'Dh', Dh, ...
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'Dm', Dm ...
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);
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initializeInputs(opts_inputs);
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%% Initialize SolidWorks Data
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initializeSolids();
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%% Initialize Ground
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initializeGround();
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@ -2,4 +2,4 @@
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clear; close all; clc;
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%%
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sim('Micro_Station_Displacement.slx');
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sim('sim_nano_station_disp.slx');
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BIN
demonstration/sim_nano_station_disp.slx
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BIN
demonstration/sim_nano_station_disp.slx
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@ -13,7 +13,7 @@ options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'sim_micro_station';
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mdl = 'sim_micro_station_id';
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%% Micro-Hexapod
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% Input/Output definition
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@ -11,7 +11,7 @@ options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'sim_micro_station';
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mdl = 'sim_micro_station_id';
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%% Micro-Hexapod
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% Input/Output definition
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@ -13,7 +13,7 @@ options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'sim_nano_station';
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mdl = 'sim_nano_station_id';
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%% Y-Translation Stage
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% Input/Output definition
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identification/sim_micro_station_id.slx
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identification/sim_micro_station_id.slx
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BIN
identification/sim_nano_station_id.slx
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identification/sim_nano_station_id.slx
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@ -11,15 +11,12 @@ initializeSimConf(opts_sim);
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%% Initialize Inputs
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opts_inputs = struct(...
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'Dw', true, ...
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'ry', false, ...
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'Ry', false, ...
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'Rz', true ...
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);
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initializeInputs(opts_inputs);
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%% Initialize Solids
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initializeSolids();
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%% Initialize Ground
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initializeGround();
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@ -5,13 +5,15 @@
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load('./mat/sim_conf.mat');
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%% Load SolidWorks Data
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load('./mat/solids.mat');
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% load('./mat/solids.mat');
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%% Load data of each stage
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load('./mat/stages.mat');
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% TODO - This is now loaded by mask of each stage
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% load('./mat/stages.mat');
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%% Load Signals Applied to the system
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load('./mat/inputs.mat');
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% TODO - This is now loaded by the input referenced system
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% load('./mat/inputs.mat');
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%% Load Controller
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load('./mat/controllers.mat');
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@ -2,7 +2,27 @@ function [axisc] = initializeAxisc()
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%%
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axisc = struct();
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axisc.m = 40; % [kg]
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%% Axis Compensator - Static Properties
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% Structure
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axisc.structure.density = 3400; % [kg/m3]
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axisc.structure.color = [0.792 0.820 0.933];
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axisc.structure.STEP = './STEPS/axisc/axisc_structure.STEP';
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% Wheel
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axisc.wheel.density = 2700; % [kg/m3]
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axisc.wheel.color = [0.753 0.753 0.753];
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axisc.wheel.STEP = './STEPS/axisc/axisc_wheel.STEP';
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% Mass
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axisc.mass.density = 7800; % [kg/m3]
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axisc.mass.color = [0.792 0.820 0.933];
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axisc.mass.STEP = './STEPS/axisc/axisc_mass.STEP';
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% Gear
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axisc.gear.density = 7800; % [kg/m3]
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axisc.gear.color = [0.792 0.820 0.933];
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axisc.gear.STEP = './STEPS/axisc/axisc_gear.STEP';
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axisc.m = 40; % TODO [kg]
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%% Axis Compensator - Dynamical Properties
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axisc.k.ax = 1; % TODO [N*m/deg)]
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axisc.c.ax = (1/1)*sqrt(axisc.k.ax/axisc.m);
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@ -2,8 +2,14 @@ function [granite] = initializeGranite()
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%%
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granite = struct();
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granite.m = 2000; % [kg]
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%% Static Properties
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granite.density = 2800; % [kg/m3]
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granite.volume = 0.72; % [m3] TODO - should
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granite.mass = granite.density*granite.volume; % [kg]
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granite.color = [1 1 1];
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granite.STEP = './STEPS/granite/granite.STEP';
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%% Dynamical Properties
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granite.k.x = 1e8; % [N/m]
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granite.c.x = 1e4; % [N/(m/s)]
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@ -101,10 +101,11 @@ function [inputs] = initializeInputs(opts_param)
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Fg = zeros(length(t), 3);
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%% External Forces applied on the Sample
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Fs = zeros(length(t), 3);
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Fs = zeros(length(t), 6);
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%% Create the input Structure that will contain all the inputs
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inputs = struct( ...
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'Ts', sim_conf.Ts, ...
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'Dw', timeseries(Dw, t), ...
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'Dy', timeseries(Dy, t), ...
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'Ry', timeseries(Ry, t), ...
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@ -22,6 +22,7 @@ function [] = initializeMirror(opts_param)
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mirror.rad = 180; % radius of the mirror (at the bottom surface) [mm]
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mirror.density = 2400; % Density of the mirror [kg/m3]
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mirror.color = [0.4 1.0 1.0]; % Color of the mirror
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mirror.cone_length = mirror.rad*tand(opts.angle)+mirror.h+mirror.jacobian; % Distance from Apex point of the cone to jacobian point
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@ -12,8 +12,27 @@ function [ry] = initializeRy(opts_param)
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%%
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ry = struct();
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ry.m = 200; % [kg]
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%% Tilt Stage - Static Properties
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% Ry - Guide for the tilt stage
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ry.guide.density = 7800; % [kg/m3]
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ry.guide.color = [0.792 0.820 0.933];
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ry.guide.STEP = './STEPS/ry/Tilt_Guide.STEP';
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% Ry - Rotor of the motor
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ry.rotor.density = 2400; % [kg/m3]
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ry.rotor.color = [0.792 0.820 0.933];
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ry.rotor.STEP = './STEPS/ry/Tilt_Motor_Axis.STEP';
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% Ry - Motor
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ry.motor.density = 3200; % [kg/m3]
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ry.motor.color = [0.792 0.820 0.933];
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ry.motor.STEP = './STEPS/ry/Tilt_Motor.STEP';
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% Ry - Plateau Tilt
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ry.stage.density = 7800; % [kg/m3]
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ry.stage.color = [0.792 0.820 0.933];
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ry.stage.STEP = './STEPS/ry/Tilt_Stage.STEP';
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ry.m = 200; % TODO [kg]
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%% Tilt Stage - Dynamical Properties
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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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else
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@ -12,9 +12,24 @@ function [rz] = initializeRz(opts_param)
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%%
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rz = struct();
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%% Spindle - Static Properties
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% Spindle - Slip Ring
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rz.slipring.density = 7800; % [kg/m3]
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rz.slipring.color = [0.792 0.820 0.933];
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rz.slipring.STEP = './STEPS/rz/Spindle_Slip_Ring.STEP';
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% Spindle - Rotor
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rz.rotor.density = 7800; % [kg/m3]
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rz.rotor.color = [0.792 0.820 0.933];
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rz.rotor.STEP = './STEPS/rz/Spindle_Rotor.STEP';
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% Spindle - Stator
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rz.stator.density = 7800; % [kg/m3]
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rz.stator.color = [0.792 0.820 0.933];
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rz.stator.STEP = './STEPS/rz/Spindle_Stator.STEP';
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% Estimated mass of the mooving part
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rz.m = 250; % [kg]
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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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function [solids] = initializeSolids()
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%% Granite
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solids.granite.density = 2800; % [kg/m3]
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solids.granite.color = [1 1 1];
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solids.granite.STEP = './STEPS/granite/granite.STEP';
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%% Y-Translation
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% Ty Granite frame
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solids.ty.granite_frame.density = 7800; % [kg/m3]
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solids.ty.granite_frame.color = [0.753 1 0.753];
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solids.ty.granite_frame.STEP = './STEPS/Ty/Ty_Granite_Frame.STEP';
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% Guide Translation Ty
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solids.ty.guide.density = 7800; % [kg/m3]
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solids.ty.guide.color = [0.792 0.820 0.933];
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solids.ty.guide.STEP = './STEPS/ty/Ty_Guide.STEP';
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% Ty - Guide_Translation12
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solids.ty.guide12.density = 7800; % [kg/m3]
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solids.ty.guide12.color = [0.792 0.820 0.933];
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solids.ty.guide12.STEP = './STEPS/Ty/Ty_Guide_12.STEP';
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% Ty - Guide_Translation11
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solids.ty.guide11.density = 7800; % [kg/m3]
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solids.ty.guide11.color = [0.792 0.820 0.933];
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solids.ty.guide11.STEP = './STEPS/ty/Ty_Guide_11.STEP';
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% Ty - Guide_Translation22
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solids.ty.guide22.density = 7800; % [kg/m3]
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solids.ty.guide22.color = [0.792 0.820 0.933];
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solids.ty.guide22.STEP = './STEPS/ty/Ty_Guide_22.STEP';
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% Ty - Guide_Translation21
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solids.ty.guide21.density = 7800; % [kg/m3]
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solids.ty.guide21.color = [0.792 0.820 0.933];
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solids.ty.guide21.STEP = './STEPS/Ty/Ty_Guide_21.STEP';
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% Ty - Plateau translation
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solids.ty.frame.density = 7800; % [kg/m3]
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solids.ty.frame.color = [0.792 0.820 0.933];
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solids.ty.frame.STEP = './STEPS/ty/Ty_Stage.STEP';
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% Ty Stator Part
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solids.ty.stator.density = 5400; % [kg/m3]
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solids.ty.stator.color = [0.792 0.820 0.933];
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solids.ty.stator.STEP = './STEPS/ty/Ty_Motor_Stator.STEP';
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% Ty Rotor Part
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solids.ty.rotor.density = 5400; % [kg/m3]
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solids.ty.rotor.color = [0.792 0.820 0.933];
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solids.ty.rotor.STEP = './STEPS/ty/Ty_Motor_Rotor.STEP';
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%% Tilt Stage
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% Ry - Guide for the tilt stage
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solids.ry.guide.density = 7800; % [kg/m3]
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solids.ry.guide.color = [0.792 0.820 0.933];
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solids.ry.guide.STEP = './STEPS/ry/Tilt_Guide.STEP';
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% Ry - Rotor of the motor
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solids.ry.rotor.density = 2400; % [kg/m3]
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solids.ry.rotor.color = [0.792 0.820 0.933];
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solids.ry.rotor.STEP = './STEPS/ry/Tilt_Motor_Axis.STEP';
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% Ry - Motor
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solids.ry.motor.density = 3200; % [kg/m3]
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solids.ry.motor.color = [0.792 0.820 0.933];
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solids.ry.motor.STEP = './STEPS/ry/Tilt_Motor.STEP';
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% Ry - Plateau Tilt
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solids.ry.stage.density = 7800; % [kg/m3]
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solids.ry.stage.color = [0.792 0.820 0.933];
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solids.ry.stage.STEP = './STEPS/ry/Tilt_Stage.STEP';
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%% Spindle
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% Spindle - Slip Ring
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solids.rz.slipring.density = 7800; % [kg/m3]
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solids.rz.slipring.color = [0.792 0.820 0.933];
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solids.rz.slipring.STEP = './STEPS/rz/Spindle_Slip_Ring.STEP';
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% Spindle - Rotor
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solids.rz.rotor.density = 7800; % [kg/m3]
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solids.rz.rotor.color = [0.792 0.820 0.933];
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solids.rz.rotor.STEP = './STEPS/rz/Spindle_Rotor.STEP';
|
||||
% Spindle - Stator
|
||||
solids.rz.stator.density = 7800; % [kg/m3]
|
||||
solids.rz.stator.color = [0.792 0.820 0.933];
|
||||
solids.rz.stator.STEP = './STEPS/rz/Spindle_Stator.STEP';
|
||||
|
||||
%% Axis Compensator
|
||||
% Structure
|
||||
solids.axisc.structure.density = 3400; % [kg/m3]
|
||||
solids.axisc.structure.color = [0.792 0.820 0.933];
|
||||
solids.axisc.structure.STEP = './STEPS/axisc/axisc_structure.STEP';
|
||||
% Wheel
|
||||
solids.axisc.wheel.density = 2700; % [kg/m3]
|
||||
solids.axisc.wheel.color = [0.753 0.753 0.753];
|
||||
solids.axisc.wheel.STEP = './STEPS/axisc/axisc_wheel.STEP';
|
||||
% Mass
|
||||
solids.axisc.mass.density = 7800; % [kg/m3]
|
||||
solids.axisc.mass.color = [0.792 0.820 0.933];
|
||||
solids.axisc.mass.STEP = './STEPS/axisc/axisc_mass.STEP';
|
||||
% Gear
|
||||
solids.axisc.gear.density = 7800; % [kg/m3]
|
||||
solids.axisc.gear.color = [0.792 0.820 0.933];
|
||||
solids.axisc.gear.STEP = './STEPS/axisc/axisc_gear.STEP';
|
||||
|
||||
%% Save
|
||||
save('./mat/solids.mat', 'solids')
|
||||
end
|
@ -12,8 +12,47 @@ function [ty] = initializeTy(opts_param)
|
||||
%%
|
||||
ty = struct();
|
||||
|
||||
ty.m = 250; % [kg]
|
||||
%% Y-Translation - Static Properties
|
||||
% Ty Granite frame
|
||||
ty.granite_frame.density = 7800; % [kg/m3]
|
||||
ty.granite_frame.color = [0.753 1 0.753];
|
||||
ty.granite_frame.STEP = './STEPS/Ty/Ty_Granite_Frame.STEP';
|
||||
% Guide Translation Ty
|
||||
ty.guide.density = 7800; % [kg/m3]
|
||||
ty.guide.color = [0.792 0.820 0.933];
|
||||
ty.guide.STEP = './STEPS/ty/Ty_Guide.STEP';
|
||||
% Ty - Guide_Translation12
|
||||
ty.guide12.density = 7800; % [kg/m3]
|
||||
ty.guide12.color = [0.792 0.820 0.933];
|
||||
ty.guide12.STEP = './STEPS/Ty/Ty_Guide_12.STEP';
|
||||
% Ty - Guide_Translation11
|
||||
ty.guide11.density = 7800; % [kg/m3]
|
||||
ty.guide11.color = [0.792 0.820 0.933];
|
||||
ty.guide11.STEP = './STEPS/ty/Ty_Guide_11.STEP';
|
||||
% Ty - Guide_Translation22
|
||||
ty.guide22.density = 7800; % [kg/m3]
|
||||
ty.guide22.color = [0.792 0.820 0.933];
|
||||
ty.guide22.STEP = './STEPS/ty/Ty_Guide_22.STEP';
|
||||
% Ty - Guide_Translation21
|
||||
ty.guide21.density = 7800; % [kg/m3]
|
||||
ty.guide21.color = [0.792 0.820 0.933];
|
||||
ty.guide21.STEP = './STEPS/Ty/Ty_Guide_21.STEP';
|
||||
% Ty - Plateau translation
|
||||
ty.frame.density = 7800; % [kg/m3]
|
||||
ty.frame.color = [0.792 0.820 0.933];
|
||||
ty.frame.STEP = './STEPS/ty/Ty_Stage.STEP';
|
||||
% Ty Stator Part
|
||||
ty.stator.density = 5400; % [kg/m3]
|
||||
ty.stator.color = [0.792 0.820 0.933];
|
||||
ty.stator.STEP = './STEPS/ty/Ty_Motor_Stator.STEP';
|
||||
% Ty Rotor Part
|
||||
ty.rotor.density = 5400; % [kg/m3]
|
||||
ty.rotor.color = [0.792 0.820 0.933];
|
||||
ty.rotor.STEP = './STEPS/ty/Ty_Motor_Rotor.STEP';
|
||||
|
||||
ty.m = 250; % TODO [kg]
|
||||
|
||||
%% Y-Translation - Dynamicals Properties
|
||||
if opts.rigid
|
||||
ty.k.ax = 1e10; % Axial Stiffness for each of the 4 guidance (y) [N/m]
|
||||
else
|
||||
|
BIN
mat/config.mat
BIN
mat/config.mat
Binary file not shown.
Binary file not shown.
Binary file not shown.
BIN
mat/inputs.mat
BIN
mat/inputs.mat
Binary file not shown.
BIN
mat/sim_conf.mat
BIN
mat/sim_conf.mat
Binary file not shown.
BIN
mat/solids.mat
BIN
mat/solids.mat
Binary file not shown.
BIN
mat/stages.mat
BIN
mat/stages.mat
Binary file not shown.
BIN
nass_library/QuaternionToAngles.slx
Normal file
BIN
nass_library/QuaternionToAngles.slx
Normal file
Binary file not shown.
BIN
nass_library/RotationMatrixToAngle.slx
Normal file
BIN
nass_library/RotationMatrixToAngle.slx
Normal file
Binary file not shown.
Binary file not shown.
Binary file not shown.
Binary file not shown.
@ -3,17 +3,17 @@ steady_time = 10;
|
||||
|
||||
initializeSimConf(struct('Tsim', steady_time, 'cl_time', steady_time));
|
||||
|
||||
set_param('Assemblage',...
|
||||
set_param('sim_nano_station_ctrl',...
|
||||
'SaveFinalState','on',...
|
||||
'FinalStateName','myOperPoint',...
|
||||
'SaveCompleteFinalSimState','on'...
|
||||
);
|
||||
|
||||
sim('Assemblage');
|
||||
sim('sim_nano_station_ctrl');
|
||||
|
||||
save('./data/myOperPoint.mat', 'myOperPoint');
|
||||
|
||||
set_param('Assemblage',...
|
||||
set_param('sim_nano_station_ctrl',...
|
||||
'SaveFinalState','off',...
|
||||
'SaveCompleteFinalSimState','off'...
|
||||
);
|
||||
@ -27,14 +27,14 @@ initializeSimConf(struct('Tsim', steady_time+sim_time, 'cl_time', steady_time));
|
||||
|
||||
load('./data/myOperPoint.mat', 'myOperPoint');
|
||||
|
||||
set_param('Assemblage',...
|
||||
set_param('sim_nano_station_ctrl',...
|
||||
'LoadInitialState','on',...
|
||||
'InitialState','myOperPoint'...
|
||||
);
|
||||
|
||||
sim('Assemblage');
|
||||
sim('sim_nano_station_ctrl');
|
||||
|
||||
set_param('Assemblage',...
|
||||
set_param('sim_nano_station_ctrl',...
|
||||
'LoadInitialState','off' ...
|
||||
);
|
||||
|
||||
|
BIN
sim_nano_station_ctrl.slx
Normal file
BIN
sim_nano_station_ctrl.slx
Normal file
Binary file not shown.
@ -14,29 +14,36 @@ function [sys] = identifyPlant(opts_param)
|
||||
options.SampleTime = 0;
|
||||
|
||||
%% Name of the Simulink File
|
||||
mdl = 'sim_nano_station';
|
||||
mdl = 'sim_nano_station_id';
|
||||
|
||||
%% Input/Output definition
|
||||
io(1) = linio([mdl, '/Fn'], 1, 'input');
|
||||
io(2) = linio([mdl, '/Gm'], 1, 'input');
|
||||
io(3) = linio([mdl, '/Fs_ext'], 1, 'input');
|
||||
io(4) = linio([mdl, '/F_legs'], 1, 'input');
|
||||
io(5) = linio([mdl, '/Dsample_meas'], 1, 'output');
|
||||
io(6) = linio([mdl, '/F_meas'], 1, 'output');
|
||||
io(1) = linio([mdl, '/Fn'], 1, 'input'); % Cartesian forces applied by NASS
|
||||
io(2) = linio([mdl, '/Dw'], 1, 'input'); % Ground Motion
|
||||
io(3) = linio([mdl, '/Fs'], 1, 'input'); % External forces on the sample
|
||||
io(4) = linio([mdl, '/Fnl'], 1, 'input'); % Forces applied on the NASS's legs
|
||||
io(5) = linio([mdl, '/Dsm'], 1, 'output'); % Displacement of the sample
|
||||
io(6) = linio([mdl, '/Fnlm'], 1, 'output'); % Force sensor in NASS's legs
|
||||
io(7) = linio([mdl, '/Dnlm'], 1, 'output'); % Displacement of NASS's legs
|
||||
|
||||
%% Run the linearization
|
||||
G = linearize(mdl, io, 0);
|
||||
G.InputName = {'Fnx', 'Fny', 'Fnz', 'Mnx', 'Mny', 'Mnz', ...
|
||||
'Dgx', 'Dgy', 'Dgz', ...
|
||||
'Fsx', 'Fsy', 'Fsz', ...
|
||||
'Fsx', 'Fsy', 'Fsz', 'Msx', 'Msy', 'Msz', ...
|
||||
'F1', 'F2', 'F3', 'F4', 'F5', 'F6'};
|
||||
G.OutputName = {'Dx', 'Dy', 'Dz', 'Rx', 'Ry', 'Rz', ...
|
||||
'Fm1', 'Fm2', 'Fm3', 'Fm4', 'Fm5', 'Fm6'};
|
||||
'Fm1', 'Fm2', 'Fm3', 'Fm4', 'Fm5', 'Fm6', ...
|
||||
'Dm1', 'Dm2', 'Dm3', 'Dm4', 'Dm5', 'Dm6'};
|
||||
|
||||
%% Create the sub transfer functions
|
||||
% From forces applied in the cartesian frame to displacement of the sample in the cartesian frame
|
||||
sys.G_cart = minreal(G({'Dx', 'Dy', 'Dz', 'Rx', 'Ry', 'Rz'}, {'Fnx', 'Fny', 'Fnz', 'Mnx', 'Mny', 'Mnz'}));
|
||||
% From ground motion to Sample displacement
|
||||
sys.G_gm = minreal(G({'Dx', 'Dy', 'Dz', 'Rx', 'Ry', 'Rz'}, {'Dgx', 'Dgy', 'Dgz'}));
|
||||
sys.G_fs = minreal(G({'Dx', 'Dy', 'Dz', 'Rx', 'Ry', 'Rz'}, {'Fsx', 'Fsy', 'Fsz'}));
|
||||
% From direct forces applied on the sample to displacement of the sample
|
||||
sys.G_fs = minreal(G({'Dx', 'Dy', 'Dz', 'Rx', 'Ry', 'Rz'}, {'Fsx', 'Fsy', 'Fsz', 'Msx', 'Msy', 'Msz'}));
|
||||
% From forces applied on NASS's legs to force sensor in each leg
|
||||
sys.G_iff = minreal(G({'Fm1', 'Fm2', 'Fm3', 'Fm4', 'Fm5', 'Fm6'}, {'F1', 'F2', 'F3', 'F4', 'F5', 'F6'}));
|
||||
% From forces applied on NASS's legs to displacement of each leg
|
||||
sys.G_dleg = minreal(G({'Dm1', 'Dm2', 'Dm3', 'Dm4', 'Dm5', 'Dm6'}, {'F1', 'F2', 'F3', 'F4', 'F5', 'F6'}));
|
||||
end
|
||||
|
||||
|
@ -43,7 +43,7 @@ function [] = runSimulation(sys_name, sys_mass, ctrl_type, act_damp)
|
||||
end
|
||||
|
||||
%% Run the simulation
|
||||
sim('Assemblage.slx');
|
||||
sim('sim_nano_station_ctrl.slx');
|
||||
|
||||
%% Split the Dsample matrix into vectors
|
||||
[Dx, Dy, Dz, Rx, Ry, Rz] = matSplit(Dsample.Data, 1); %#ok
|
||||
|
Binary file not shown.
Loading…
Reference in New Issue
Block a user