diff --git a/common b/common
index 7eab42722e6f7e0576f77383b27bfcd614096e88..59b6c1b09cbd9b1bc1be07e1aa32f18ced11e1bc 160000
--- a/common
+++ b/common
@@ -1 +1 @@
-Subproject commit 7eab42722e6f7e0576f77383b27bfcd614096e88
+Subproject commit 59b6c1b09cbd9b1bc1be07e1aa32f18ced11e1bc
diff --git a/simulator/src/prints.m b/simulator/src/prints.m
index 599b37c96e1002df1624277378889a29731d9757..345c1f51e1b9dec7886fde258fa272b40f900b9e 100644
--- a/simulator/src/prints.m
+++ b/simulator/src/prints.m
@@ -66,9 +66,7 @@ maxTemperature = (externalTemp*(1+(((gamma-1)/2)*(mach(iMaxV)^2))))-273.15;
 %     XCPor = ascent.coeff.XCPor(~isnan(ascent.coeff.XCPor)); % keeping the NaN elements in ascent.coeff.XCPor, but not in XCPor
 % end
 
-% longitudinal XCPs
-lonXCPs = -ascent.coeff.XCPlon(~isnan(ascent.coeff.XCPlon));
-latXCPs = -ascent.coeff.XCPlat(~isnan(ascent.coeff.XCPlat));
+% XCP
 totXCPs = ascent.coeff.XCPtot(~isnan(ascent.coeff.XCPtot));
 
 % DATA RECORD (display)
@@ -101,7 +99,7 @@ fprintf('speed at launch pad exit: %g [m/s] \n', absV(iExit))
 % else
 %     fprintf('Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n', lonXCPs(1), latXCPs(1), totXCPs(1))
 % end
-fprintf('Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n', lonXCPs(1), latXCPs(1), totXCPs(1))
+fprintf('Stability margin at launchpad exit [-]:\n Lon: %g\n Lat: %g\n Tot: %g\n', totXCPs(1))
 fprintf('time: %g [sec] \n\n', time(iExit))
 
 fprintf('latitude of landing point: %10.8f [deg] \n', lat(end));