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Commit 5d4dfc91 authored by giuliaghirardini's avatar giuliaghirardini Committed by Marco Luigi Gaibotti
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[refactoring-missions][2022_Pyxis_Roccaraso_September] Moved old data to old folder

parent d48ec789
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1 merge request!5Refactoring missions
......@@ -28,22 +28,22 @@ settings.Local = []; % vector [altLocal, TLoc
%% ENGINE DETAILS
% load motors data
filename = '../Motors.mat';
filename = 'D:\GitHub\msa-toolkit\common\missions\2022_Pyxis_Roccaraso_September\data\motors.mat';
load(filename);
engineName = 'L820-SK';
crossCase = false; % true if you want a Cesaroni case with an Aerotech reload, and viceversa
iMotor = [Motors.MotorName] == engineName;
settings.motor.expTime = Motors(iMotor).t;
settings.motor.expThrust = Motors(iMotor).T;
settings.motor.expM = Motors(iMotor).m;
settings.mp = Motors(iMotor).mp; % [kg] Propellant Mass
settings.tb = Motors(iMotor).t(end) ; % [s] Burning time
iMotor = 431;
settings.motor.expTime = motors(iMotor).t;
settings.motor.expThrust = motors(iMotor).T;
settings.motor.expM = motors(iMotor).m;
settings.mp = motors(iMotor).mp; % [kg] Propellant Mass
settings.tb = motors(iMotor).t(end) ; % [s] Burning time
if not(crossCase)
mc = Motors(iMotor).mc; % [kg] Case mass
mc = motors(iMotor).mc; % [kg] Case mass
else
mc = Motors(iMotor).mcCross;
mc = motors(iMotor).mcCross;
end
settings.mNoMot = 13.9;
settings.ms = settings.mNoMot + mc; % [kg] Structural Mass
......@@ -259,7 +259,7 @@ settings.prob.SafeEllipse(1).alpha = 10;
%% LANDING POINTS
% satellite maps of the landing zone
% delta limit on the coordinates (for the landing map)
settings.limLat = 0.04;
% settings.limLat = 0.04;
settings.limLon = 0.025;
......
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