diff --git a/sensitivityAnalysis/src/stochParameters/initParameter.m b/sensitivityAnalysis/src/stochParameters/initParameter.m
index f00667535ec5a68b704a5e237a045ec0ce22df05..621446fb3e12731b73adb9389d498ff5e31e0441 100644
--- a/sensitivityAnalysis/src/stochParameters/initParameter.m
+++ b/sensitivityAnalysis/src/stochParameters/initParameter.m
@@ -55,28 +55,28 @@ for i = 1:length(parameters)
parameters(i).value = rocket.inertia(3, :);
parameters(i).udm = 'kg*m^4';
case 'drogueSurface'
- parameters(i).value = rocket.parachutes(1, 1).surface;
+ parameters(i).value = rocket.parachutes{1, 1}.surface;
parameters(i).udm = 'm2';
case 'drogueMass'
- parameters(i).value = rocket.parachutes(1, 1).mass;
+ parameters(i).value = rocket.parachutes{1, 1}.mass;
parameters(i).udm = 'kg';
case 'drogueCl'
- parameters(i).value = rocket.parachutes(1, 1).cl;
+ parameters(i).value = rocket.parachutes{1, 1}.cl;
parameters(i).udm = '-';
case 'drogueCd'
- parameters(i).value = rocket.parachutes(1, 1).cd;
+ parameters(i).value = rocket.parachutes{1, 1}.cd;
parameters(i).udm = '-';
case 'mainSurface'
- parameters(i).value = rocket.parachutes(2, 1).surface;
+ parameters(i).value = rocket.parachutes{2, 1}.surface;
parameters(i).udm = 'm2';
case 'mainMass'
- parameters(i).value = rocket.parachutes(2, 1).mass;
+ parameters(i).value = rocket.parachutes{2, 1}.mass;
parameters(i).udm = 'kg';
case 'mainCl'
- parameters(i).value = rocket.parachutes(2, 1).cl;
+ parameters(i).value = rocket.parachutes{2, 1}.cl;
parameters(i).udm = '-';
case 'mainCd'
- parameters(i).value = rocket.parachutes(2, 1).cd;
+ parameters(i).value = rocket.parachutes{2, 1}.cd;
parameters(i).udm = '-';
% rocket geometry --- available with the stability run only
case 'rocketDiameter'
diff --git a/sensitivityAnalysis/src/stochParameters/updateData.m b/sensitivityAnalysis/src/stochParameters/updateData.m
index 363be07e438f4a9f39aa86af1bd13ff4fc203727..6c1c26c8f4bad79b6807f68ffb84fe9eea86abac 100644
--- a/sensitivityAnalysis/src/stochParameters/updateData.m
+++ b/sensitivityAnalysis/src/stochParameters/updateData.m
@@ -62,21 +62,21 @@ for i = 1:length(parameters)
case 'Izz'
rocket.inertia(3, :) = value;
case 'drogueSurface'
- rocket.parachutes(1, 1).surface = value;
+ rocket.parachutes{1, 1}.surface = value;
case 'drogueMass'
- rocket.parachutes(1, 1).mass = value;
+ rocket.parachutes{1, 1}.mass = value;
case 'drogueCl'
- rocket.parachutes(1, 1).cl = value;
+ rocket.parachutes{1, 1}.cl = value;
case 'drogueCd'
- rocket.parachutes(1, 1).cd = value;
+ rocket.parachutes{1, 1}.cd = value;
case 'mainSurface'
- rocket.parachutes(2, 1).surface = value;
+ rocket.parachutes{2, 1}.surface = value;
case 'mainMass'
- rocket.parachutes(2, 1).mass = value;
+ rocket.parachutes{2, 1}.mass = value;
case 'mainCl'
- rocket.parachutes(2, 1).cl = value;
+ rocket.parachutes{2, 1}.cl = value;
case 'mainCd'
- rocket.parachutes(2, 1).cd = value;
+ rocket.parachutes{2, 1}.cd = value;
% rocket geometry --- available with the stability run only
case 'rocketDiameter'
rocket.diameter = value;
diff --git a/simulator/mainSimulator.m b/simulator/mainSimulator.m
index 5a14012e66984dad38c24bb25730d63e960fc6df..b9ec897857d6eae5de45f3019d59db52b87435f9 100644
--- a/simulator/mainSimulator.m
+++ b/simulator/mainSimulator.m
@@ -51,7 +51,7 @@ if isempty(settings), settings = Settings('ode', 'simulator'); end
Settings.read(settings, options, 'simulator');
%% CHECKS
-if settings.simulator.ballistic && rocket.parachutes(end, 1).finalAltitude ~= 0
+if settings.simulator.ballistic && rocket.parachutes{end, 1}.finalAltitude ~= 0
error('The landing will be not achived, check the final altitude of the last parachute in config.m')
end
if settings.simulator.ballistic && settings.simulator.parafoil
diff --git a/simulator/src/stdPlots.m b/simulator/src/stdPlots.m
index df42c8dea503f84f02c8f7adb85918f6a682b674..6ef6d6868cfa354bcec857b3c1d35345176a06b9 100644
--- a/simulator/src/stdPlots.m
+++ b/simulator/src/stdPlots.m
@@ -182,7 +182,7 @@ if ~settings.simulator.ballistic
plots(iPlot) = plot3(xM, yM, zM, 'o',...
'MarkerSize', 10, 'MarkerFaceColor', colorMarker(:, iMarker) , 'MarkerEdgeColor', 'none');
- labels(iPlot) = strcat("Stage: ", num2str(j), " ", rocket.parachutes(i,j).name ," opening");
+ labels(iPlot) = strcat("Stage: ", num2str(j), " ", rocket.parachutes{i,j}.name ," opening");
iPlot = iPlot + 1;
iMarker = iMarker + 1;
end
@@ -301,7 +301,7 @@ if ~settings.simulator.ballistic
subplot(3, 1, 3);
plots(iPlot) = plot(tDescent, vzDescent);
- legends(iPlot) = strcat( "Stage ", num2str(j), ": ", rocket.parachutes(i, j).name , " trajectory" );
+ legends(iPlot) = strcat( "Stage ", num2str(j), ": ", rocket.parachutes{i, j}.name , " trajectory" );
iPlot = iPlot + 1;
end
end
@@ -470,7 +470,7 @@ if ~settings.simulator.ballistic
subplot(1, 3, 3);
plots(iPlot) = plot(yDescent, zDescent);
- legends(iPlot) = strcat( "Stage ", num2str(j), ": ", rocket.parachutes(i, j).name , " trajectory" );
+ legends(iPlot) = strcat( "Stage ", num2str(j), ": ", rocket.parachutes{i, j}.name , " trajectory" );
iPlot = iPlot + 1;
end
end
diff --git a/utils/rocketpyData/exportRocketpy.m b/utils/rocketpyData/exportRocketpy.m
index c7dc066a46824cfa82b00d4a5839e7da505a24a9..9c56cb1517973a111ac02b336c9ce3b87078aaf6 100644
--- a/utils/rocketpyData/exportRocketpy.m
+++ b/utils/rocketpyData/exportRocketpy.m
@@ -146,16 +146,16 @@ fins_position = rocket.lengthCenter - rocket.rear.finsAxialDistance - root_chord
boat_position = rocket.lengthCenter;
%% parachutes
-booster_drogue_cd_s = rocket.parachutes(1, 1).surface * rocket.parachutes(1, 1).cd;
-booster_drogue_opening_delay = rocket.parachutes(1,1).openingTime;
+booster_drogue_cd_s = rocket.parachutes{1, 1}.surface * rocket.parachutes{1, 1}.cd;
+booster_drogue_opening_delay = rocket.parachutes{1,1}.openingTime;
-booster_main_cd_s = rocket.parachutes(2, 1).surface * rocket.parachutes(2, 1).cd;
-booster_main_opening_delay = rocket.parachutes(2,1).openingTime;
-booster_main_opening_altitude = rocket.parachutes(1, 1).finalAltitude + environment.z0;
+booster_main_cd_s = rocket.parachutes{2, 1}.surface * rocket.parachutes{2, 1}.cd;
+booster_main_opening_delay = rocket.parachutes{2,1}.openingTime;
+booster_main_opening_altitude = rocket.parachutes{1, 1}.finalAltitude + environment.z0;
-payload_drogue_cd_s = rocket.parachutes(1, 2).surface * rocket.parachutes(1, 2).cd;
-payload_drogue_opening_delay = rocket.parachutes(1, 2).openingTime;
-parafoil_opening_altitude = rocket.parachutes(1, 2).finalAltitude + environment.z0;
+payload_drogue_cd_s = rocket.parachutes{1, 2}.surface * rocket.parachutes{1, 2}.cd;
+payload_drogue_opening_delay = rocket.parachutes{1, 2}.openingTime;
+parafoil_opening_altitude = rocket.parachutes{1, 2}.finalAltitude + environment.z0;
%% launchpad and environment details
latitude = environment.lat0;