diff --git a/sensitivityAnalysis/src/postprocess/postprocessAscent.m b/sensitivityAnalysis/src/postprocess/postprocessAscent.m
index 55dfeb58d251f6bbe6c5e3b4421843c1542092e0..c60943a450e5e5546687beb6094d30a787dc7d54 100644
--- a/sensitivityAnalysis/src/postprocess/postprocessAscent.m
+++ b/sensitivityAnalysis/src/postprocess/postprocessAscent.m
@@ -277,63 +277,52 @@ for i = 1:N
     %   - Altitude is assigned as the minimum value within the same bin.
     % This is done to capture the worst-case conditions for the structural analysis of the rocket's fins.
 
-    mach  = ascent(i).interp.mach;
-    alpha = ascent(i).interp.alpha;
-    beta  = ascent(i).interp.beta;
-    alt   = ascent(i).interp.alt;
-    indMax = find(mach == machMax(i));
-    
-    edgesAcc = mach(1):0.05:machMax(i);
-    
-    % Acceleration
-    machAcc  = mach(1:indMax);
-    alphaAcc = alpha(1:indMax);
-    betaAcc  = beta(1:indMax);
-    altAcc   = alt(1:indMax);
-    
-    alphaMaxAcc = NaN((length(edgesAcc)-1), 1);
-    betaMaxAcc  = NaN((length(edgesAcc)-1), 1);
-    altMinAcc   = NaN((length(edgesAcc)-1), 1);
+    mach0  = ascent(i).interp.mach;
+    alpha0 = ascent(i).interp.alpha;
+    beta0  = ascent(i).interp.beta;
+    alt0   = ascent(i).interp.alt;
+    indMax = find(mach0 == machMax(i));
+
+    types = ["machAccVersus", "machDecVersus"];
     
-    for j = 2:length(edgesAcc)
-        inBin = machAcc > edgesAcc(j-1) & machAcc <= edgesAcc(j);
-        if any(inBin)
-            alphaMaxAcc(j-1) = max(alphaAcc(inBin));
-            betaMaxAcc(j-1)  = max(betaAcc(inBin));
-            altMinAcc(j-1)   = min(altAcc(inBin));
+    for t = types
+        if t == "machAccVersus"
+            edges = (mach0(1):0.05:machMax(i))';
+            mach  = mach0(1:indMax);
+            alpha = alpha0(1:indMax);
+            beta  = beta0(1:indMax);
+            alt   = alt0(1:indMax);
+        else
+            edges = (machMax(i):-0.05:mach0(end))';
+            mach  = mach0((indMax+1):end);
+            alpha = alpha0((indMax+1):end);
+            beta  = beta0((indMax+1):end);
+            alt   = alt0((indMax+1):end);
         end
-    end
+
+        alphaMax = NaN((length(edges)-1), 1);
+        betaMax  = NaN((length(edges)-1), 1);
+        altMin   = NaN((length(edges)-1), 1);
         
-    % Deceleration
-    edgesDec = machMax(i):-0.05:mach(end);
+        for  k = 2:length(edges)
+            if t == "machAccVersus"
+                inBin = mach > edges(k-1) & mach <= edges(k);
+            else
+                inBin = mach < edges(k-1) & mach >= edges(k);
+            end
 
-    machDec  = mach((indMax+1):end);
-    alphaDec = alpha((indMax+1):end);
-    betaDec  = beta((indMax+1):end);
-    altDec   = alt((indMax+1):end);
-    
-    alphaMaxDec = NaN((length(edgesDec)-1), 1);
-    betaMaxDec  = NaN((length(edgesDec)-1), 1);
-    altMinDec   = NaN((length(edgesDec)-1), 1);
-    
-    for j = 2:length(edgesDec)
-        inBin = machDec < edgesDec(j-1) & machDec >= edgesDec(j);
-        if any(inBin)
-            alphaMaxDec(j-1) = max(alphaDec(inBin));
-            betaMaxDec(j-1)  = max(betaDec(inBin));
-            altMinDec(j-1)   = min(altDec(inBin));
+            if any(inBin)
+                alphaMax(k-1) = max(alpha(inBin));
+                betaMax(k-1)  = max(beta(inBin));
+                altMin(k-1)   = min(alt(inBin));
+            end
         end
-    end
-
-    machAccVersus(i).mach = edgesAcc(2:end);
-    machAccVersus(i).alpha = alphaMaxAcc*180/pi;
-    machAccVersus(i).beta = betaMaxAcc*180/pi;
-    machAccVersus(i).alt = altMinAcc;
 
-    machDecVersus(i).mach = edgesDec(2:end);
-    machDecVersus(i).alpha = alphaMaxDec*180/pi;
-    machDecVersus(i).beta = betaMaxDec*180/pi;
-    machDecVersus(i).alt = altMinDec;    
+        p.(t)(i).mach = edges(2:end);
+        p.(t)(i).alpha = alphaMax*180/pi;
+        p.(t)(i).beta = betaMax*180/pi;
+        p.(t)(i).alt = altMin;
+    end   
 end
 
 %% Saving data
@@ -401,6 +390,6 @@ end
 postp.nSim = N;
 postp.confidence = settings.sensitivity.plots.confidence;
 
-postp.machAccVersus = machAccVersus;
-postp.machDecVersus = machDecVersus;
+postp.machAccVersus = p.machAccVersus;
+postp.machDecVersus = p.machDecVersus;
 end
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