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Commit 344bfd7d authored by giuliaghirardini's avatar giuliaghirardini
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[refactoring-msa][classes] Implemented Parachute class and parachuteConfig

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classes/components/Parachute.m
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View file @ 344bfd7d
classdef Parachute
classdef Parachute < Component
%PARACHUTE Summary of this class goes here
% Detailed explanation goes here
properties
Property1
end
methods
function obj = Parachute(inputArg1,inputArg2)
%PARACHUTE Construct an instance of this class
% Detailed explanation goes here
obj.Property1 = inputArg1 + inputArg2;
name {mustBeTextScalar} = ''
surface double % [m^2] Surface
mass double % [kg] Parachute Mass
cd double % [/] Parachute Drag Coefficient
cl double % [/] Parachute Lift Coefficient
openingDelay double % [s] drogue opening delay
finalAltitude double % [m] Final altitude of the parachute
cx double % [/] Parachute Longitudinal Drag Coefficient
chordLength double % [m] Shock Chord Length
chordK double % [N/m^2] Shock Chord Elastic Constant
chordC double % [Ns/m] Shock Chord Dynamic Coefficient
m double % [m^2/s] Coefficient of the surface vs. time opening model
nf double % [/] Adimensional Opening Time
expulsionSpeed double
end
function outputArg = method1(obj,inputArg)
%METHOD1 Summary of this method goes here
% Detailed explanation goes here
outputArg = obj.Property1 + inputArg;
end
properties(Access = protected)
configName = 'parachuteConfig.m'
variableName = 'parachute'
mission Mission
end
end
missions/2024_Lyra_Roccaraso_September/config/parachuteConfig.m
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View file @ 344bfd7d
% CONFIG - This script contains information about the parachutes onboard
parachute = Parachute();
%% ROCKET CHUTES
% parachute 1
parachute.para(1, 1).name = 'DROGUE chute';
parachute.para(1, 1).surface = 1.2219; % [m^2] Surface
parachute.para(1, 1).mass = 0.15; % [kg] Parachute Mass
parachute.para(1, 1).cd = 0.96; % [/] Parachute Drag Coefficient
parachute.para(1, 1).cl = 0; % [/] Parachute Lift Coefficient
parachute.para(1, 1).openingDelay = 1; % [s] drogue opening delay
parachute.para(1, 1).finalAltitude = 350; % [m] Final altitude of the parachute
parachute.para(1, 1).cx = 1.4; % [/] Parachute Longitudinal Drag Coefficient
parachute.para(1, 1).chordLength = 1.5; % [m] Shock Chord Length
parachute.para(1, 1).chordK = 7200; % [N/m^2] Shock Chord Elastic Constant
parachute.para(1, 1).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
parachute.para(1, 1).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
parachute.para(1, 1).nf = 12; % [/] Adimensional Opening Time
parachute.para(1, 1).expulsionSpeed = 5; % [m/s] Expulsion Speed
parachute.name = 'DROGUE chute';
parachute.surface = 1.2219; % [m^2] Surface
parachute.mass = 0.15; % [kg] Parachute Mass
parachute.cd = 0.96; % [/] Parachute Drag Coefficient
parachute.cl = 0; % [/] Parachute Lift Coefficient
parachute.openingDelay = 1; % [s] drogue opening delay
parachute.finalAltitude = 350; % [m] Final altitude of the parachute
parachute.cx = 1.4; % [/] Parachute Longitudinal Drag Coefficient
parachute.chordLength = 1.5; % [m] Shock Chord Length
parachute.chordK = 7200; % [N/m^2] Shock Chord Elastic Constant
parachute.chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
parachute.m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
parachute.nf = 12; % [/] Adimensional Opening Time
parachute.expulsionSpeed = 5; % [m/s] Expulsion Speed
% parachute 2
parachute.para(2, 1).name = 'MAIN chute';
parachute.para(2, 1).surface = 7.34; % [m^2] Surface
parachute.para(2, 1).mass = 1.05; % [kg] Parachute Mass
parachute.para(2, 1).cd = 1.75; % [/] Parachute Drag Coefficient
parachute.para(2, 1).cl = 0; % [/] Parachute Lift Coefficient
parachute.para(2, 1).finalAltitude = 0; % [m] Final altitude of the parachute
parachute.para(2, 1).cx = 1.2; % [/] Parachute Longitudinal Drag Coefficient
parachute.para(2, 1).chordLength = 6; % [m] Shock Chord Length
parachute.para(2, 1).chordK = 3000; % [N/m^2] Shock Chord Elastic Constant
parachute.para(2, 1).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
parachute.para(2, 1).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
parachute.para(2, 1).nf = 8.7; % [/] Adimensional Opening Time
%% PAYLOAD CHUTES
% parachute 1
parachute.para(1, 2).name = "Payload DROGUE";
parachute.para(1, 2).surface = 0.11; % [m^2] Surface
parachute.para(1, 2).mass = 0.15; % [kg] Parachute Mass
parachute.para(1, 2).cd = 1.2; % [/] Parachute Drag Coefficient
parachute.para(1, 2).cl = 0; % [/] Parachute Lift Coefficient
parachute.para(1, 2).openingDelay = 1; % [s] drogue opening delay
parachute.para(1, 2).finalAltitude = 300; % [m] Final altitude of the parachute
parachute.para(1, 2).cx = 1.4; % [/] Parachute Longitudinal Drag Coefficient
parachute.para(1, 2).chordLength = 1.5; % [m] Shock Chord Length
parachute.para(1, 2).chordK = 7200; % [N/m^2] Shock Chord Elastic Constant
parachute.para(1, 2).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
parachute.para(1, 2).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
parachute.para(1, 2).nf = 12; % [/] Adimensional Opening Time
parachute.para(1, 2).expulsionSpeed = 10; % [m/s] Expulsion Speed
% parachute 2
parachute.para(2, 2).name = "Payload AIRFOIL";
parachute.para(2, 2).mass = 0.50; % [kg] Parachute Mass
parachute.para(2, 2).finalAltitude = 0; % [m] Final altitude of the parachute
% %% ROCKET CHUTES
% % parachute 1
% parachute.para(1, 1).name = 'DROGUE chute';
% parachute.para(1, 1).surface = 1.2219; % [m^2] Surface
% parachute.para(1, 1).mass = 0.15; % [kg] Parachute Mass
% parachute.para(1, 1).cd = 0.96; % [/] Parachute Drag Coefficient
% parachute.para(1, 1).cl = 0; % [/] Parachute Lift Coefficient
% parachute.para(1, 1).openingDelay = 1; % [s] drogue opening delay
% parachute.para(1, 1).finalAltitude = 350; % [m] Final altitude of the parachute
% parachute.para(1, 1).cx = 1.4; % [/] Parachute Longitudinal Drag Coefficient
% parachute.para(1, 1).chordLength = 1.5; % [m] Shock Chord Length
% parachute.para(1, 1).chordK = 7200; % [N/m^2] Shock Chord Elastic Constant
% parachute.para(1, 1).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
% parachute.para(1, 1).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
% parachute.para(1, 1).nf = 12; % [/] Adimensional Opening Time
% parachute.para(1, 1).expulsionSpeed = 5; % [m/s] Expulsion Speed
%
% % parachute 2
% parachute.para(2, 1).name = 'MAIN chute';
% parachute.para(2, 1).surface = 7.34; % [m^2] Surface
% parachute.para(2, 1).mass = 1.05; % [kg] Parachute Mass
% parachute.para(2, 1).cd = 1.75; % [/] Parachute Drag Coefficient
% parachute.para(2, 1).cl = 0; % [/] Parachute Lift Coefficient
% parachute.para(2, 1).finalAltitude = 0; % [m] Final altitude of the parachute
% parachute.para(2, 1).cx = 1.2; % [/] Parachute Longitudinal Drag Coefficient
% parachute.para(2, 1).chordLength = 6; % [m] Shock Chord Length
% parachute.para(2, 1).chordK = 3000; % [N/m^2] Shock Chord Elastic Constant
% parachute.para(2, 1).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
% parachute.para(2, 1).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
% parachute.para(2, 1).nf = 8.7; % [/] Adimensional Opening Time
%
% %% PAYLOAD CHUTES
% % parachute 1
% parachute.para(1, 2).name = "Payload DROGUE";
% parachute.para(1, 2).surface = 0.11; % [m^2] Surface
% parachute.para(1, 2).mass = 0.15; % [kg] Parachute Mass
% parachute.para(1, 2).cd = 1.2; % [/] Parachute Drag Coefficient
% parachute.para(1, 2).cl = 0; % [/] Parachute Lift Coefficient
% parachute.para(1, 2).openingDelay = 1; % [s] drogue opening delay
% parachute.para(1, 2).finalAltitude = 300; % [m] Final altitude of the parachute
% parachute.para(1, 2).cx = 1.4; % [/] Parachute Longitudinal Drag Coefficient
% parachute.para(1, 2).chordLength = 1.5; % [m] Shock Chord Length
% parachute.para(1, 2).chordK = 7200; % [N/m^2] Shock Chord Elastic Constant
% parachute.para(1, 2).chordC = 0; % [Ns/m] Shock Chord Dynamic Coefficient
% parachute.para(1, 2).m = 1; % [m^2/s] Coefficient of the surface vs. time opening model
% parachute.para(1, 2).nf = 12; % [/] Adimensional Opening Time
% parachute.para(1, 2).expulsionSpeed = 10; % [m/s] Expulsion Speed
%
% % parachute 2
% parachute.para(2, 2).name = "Payload AIRFOIL";
% parachute.para(2, 2).mass = 0.50; % [kg] Parachute Mass
% parachute.para(2, 2).finalAltitude = 0; % [m] Final altitude of the parachute
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