diff --git a/sensitivityAnalysis/src/plots/stabilityPlots.m b/sensitivityAnalysis/src/plots/stabilityPlots.m
index aa8d1857104c760438854e6a0e725400e53dbf03..563c77b4d430f52c003f9d2216fa1351bbecee44 100644
--- a/sensitivityAnalysis/src/plots/stabilityPlots.m
+++ b/sensitivityAnalysis/src/plots/stabilityPlots.m
@@ -28,21 +28,6 @@ ylabel('n cases');
 title('Rocket velocity at launchpad exit');
 
 %% Stability Margin
-nFig = nFig + 1;
-figure(nFig)
-histogram(postpStab.XCPlon.value(1, :));
-ylabel('n cases');
-xlabel('Stability margin (body calibers)');
-grid on;
-title('LONGITUDINAL Stability margin at launchpad exit')
-
-nFig = nFig + 1;
-figure(nFig)
-histogram(postpStab.XCPlat.value(1, :));
-ylabel('n cases');
-xlabel('Stability margin (body calibers)');
-grid on;
-title('DIRECTIONAL Stability margin at launchpad exit')
 
 nFig = nFig + 1;
 figure(nFig)
diff --git a/simulator/src/designPlots.m b/simulator/src/designPlots.m
index 68c77c787544d00ff1d860c19dc568e1115ed8d0..8397cb498de0c092910f6c702fad4d2c267c30ba 100644
--- a/simulator/src/designPlots.m
+++ b/simulator/src/designPlots.m
@@ -10,13 +10,11 @@ end
 tAscent = ascent.state.time;
 
 %%% Stability Margin
-figure('Name','Stability Margins - ascent Phase','NumberTitle','off');
-plot(tAscent, -ascent.coeff.XCPlon, '.',...
-    tAscent, -ascent.coeff.XCPlat, '.',...
-    tAscent, ascent.coeff.XCPtot, '.');
+figure('Name','Stability Margin - ascent Phase','NumberTitle','off');
+plot(tAscent, ascent.coeff.XCPtot, '.');
 
 title('Stability margin vs time'), grid on;
-legend('Longitudinal', 'Lateral', 'Total')
+legend('Total stability margin')
 xlabel('Time (s)'); ylabel('S.M.(/)')
 ylim([0 6.5])
 end
\ No newline at end of file
diff --git a/simulator/src/stdPlots.m b/simulator/src/stdPlots.m
index 6ef6d6868cfa354bcec857b3c1d35345176a06b9..858be91171553b4743bb17c8673099205cc696bc 100644
--- a/simulator/src/stdPlots.m
+++ b/simulator/src/stdPlots.m
@@ -42,13 +42,11 @@ nParachutes = height(rocket.parachutes);
 
 %% ASCENT PLOTS
 %%% Stability Margin
-figure('Name','Stability Margins - ascent Phase','NumberTitle','off');
-plot(tAscent, -ascent.coeff.XCPlon, '.',...
-    tAscent, -ascent.coeff.XCPlat, '.',...
-    tAscent, ascent.coeff.XCPtot, '.');
+figure('Name','Stability Margin - ascent Phase','NumberTitle','off');
+plot(tAscent, ascent.coeff.XCPtot, '.');
 
 title('Stability margin vs time'), grid on;
-legend('Longitudinal', 'Lateral', 'Total')
+legend('Total stability margin')
 xlabel('Time (s)'); ylabel('S.M.(/)')
 
 %%% Aero Forces