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Commit 76a4a5bb authored by giuliaghirardini's avatar giuliaghirardini
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[design-updates][2024_Lyra_Portugal_October] Updated Euroc data

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1 merge request!11Merge of post preliminary design changes into main
......@@ -4,11 +4,11 @@
environment = Environment();
environment.lat0 = 39.388727; % [deg] Launchpad latitude
environment.lon0 = -8.287842; % [deg] Launchpad longitude
environment.lat0 = 39.3901711000000; % [deg] Launchpad latitude
environment.lon0 = -8.28954220000000; % [deg] Launchpad longitude
environment.z0 = 160; % [m] Launchpad Altitude
environment.omega = 85; % [deg] Launchpad elevation
environment.phi = 133; % [deg] Launchpad azimuth
environment.omega = 84; % [deg] Launchpad elevation
environment.phi = 134.5; % [deg] Launchpad azimuth
environment.pin1Length = 0.5603; % [m] Distance from the upper pin to the upper tank cap
environment.pin2Length = 0.2055; % [m] Distance from the lower pin to the lower tank cap
environment.rampLength = 12; % [m] Total launchpad length
......
......@@ -49,7 +49,7 @@ airbrakes.mass = 0.936; % [kg] Tota
airbrakes.inertia = 1e-9*[3086650; 1931082; 1889047]; % [kg*m^2] Total bay inertia (Body reference)
airbrakes.xCg = 30.54 * 1e-3; % [m] Cg relative to bay upper side
airbrakes.enabled = false; % If true, multiple and smooth airbrakes opening will be simulated
airbrakes.enabled = true; % If true, multiple and smooth airbrakes opening will be simulated
airbrakes.extension = [1]; % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
airbrakes.deltaTime = [0]; % aerobrakes, configurations usage time
......@@ -95,7 +95,7 @@ motor = Motor();
% motor.name = 'HRE_ARM_P_67_T015_T03';
%
% motor.name = 'HRE_ARM_P_40_T030_T03';
motor.name = 'HRE_ARM_P_41_T030_T03';
% motor.name = 'HRE_ARM_P_41_T030_T03';
% motor.name = 'HRE_ARM_P_42_T030_T03';
% motor.name = 'HRE_ARM_P_43_T030_T03';
% motor.name = 'HRE_ARM_P_44_T030_T03';
......@@ -105,7 +105,7 @@ motor.name = 'HRE_ARM_P_41_T030_T03';
% motor.name = 'HRE_ARM_P_48_T030_T03';
% motor.name = 'HRE_ARM_P_49_T030_T03';
% motor.name = 'HRE_ARM_P_50_T030_T03';
% motor.name = 'HRE_ARM_P_52_T030_T03';
motor.name = 'HRE_ARM_P_52_T030_T03';
% motor.name = 'HRE_ARM_P_53_T030_T03';
% motor.name = 'HRE_ARM_P_54_T030_T03';
% motor.name = 'HRE_ARM_P_55_T030_T03';
......
......@@ -11,13 +11,13 @@
windCustom = WindCustom();
windCustom.altitudes = [0 140 500 1000 1500 2000 2500 3000 3500 4000]; % [m] Altitudes at which a distribution change occurs
windCustom.magnitudeDistribution = ["u", "g", "g", "g", "g", "g", "g", "g", "g", "g"]; % [-] Distribution type: "u" - uniform, "g" - gaussian
windCustom.magnitudeParameters = [0 7 12 13 13 14 14 15 15 15;
8.7 1.5 3 3 3 3 3 3 3 3]; % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
windCustom.altitudes = [0 150 500 1000 1500 2000 2500 3000 3500 4000]; % [m] Altitudes at which a distribution change occurs
windCustom.magnitudeDistribution = ["g", "g", "g", "g", "g", "g", "g", "g", "g", "g"]; % [-] Distribution type: "u" - uniform, "g" - gaussian
windCustom.magnitudeParameters = [3 4 6 7 8 11 12 14 15 18;
1.5 1.5 2 2 2 2 2 2 2 2]; % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
windCustom.azimuthDistribution = ["u", "u", "u", "u", "u", "u", "u", "u", "u", "u"]; % [-] Distribution type: "u" - uniform, "g" - gaussian
windCustom.azimuthParameters = [270 270 270 280 270 260 260 240 240 240;
290 290 290 300 290 280 280 280 280 280]*pi/180; % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
windCustom.azimuthParameters = [197 150 160 180 200 200 200 200 200 210;
217 170 180 200 220 220 220 220 220 230]*pi/180; % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
% windCustom.altitudes = [0 4500];
% windCustom.magnitudeDistribution = ["u", "u"];
......
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