From 72133740a46a982d16c9e3f1f1eda88c3e77fe08 Mon Sep 17 00:00:00 2001
From: Mauco03 <marco.gaibotti@skywarder.eu>
Date: Thu, 12 Dec 2024 22:19:03 +0100
Subject: [PATCH] [coefficients] Removing xcpLon and xcpLat from plots

---
 simulator/mainSimulator.m | 2 +-
 simulator/src/prints.m    | 9 +++++----
 2 files changed, 6 insertions(+), 5 deletions(-)

diff --git a/simulator/mainSimulator.m b/simulator/mainSimulator.m
index b9ec8978..39d184ab 100644
--- a/simulator/mainSimulator.m
+++ b/simulator/mainSimulator.m
@@ -90,5 +90,5 @@ toc(tStart)
 
 if settings.simulator.prints, prints(ascent, descent, environment); end
 if settings.simulator.plots, stdPlots(ascent, descent, rocket, environment, settings); end
-if settings.simulator.SMonly, designPlots(ascent, descent, rocket, environment, settings); end
+%if settings.simulator.SMonly, designPlots(ascent, descent, rocket, environment, settings); end
 end
\ No newline at end of file
diff --git a/simulator/src/prints.m b/simulator/src/prints.m
index 599b37c9..38bacbf0 100644
--- a/simulator/src/prints.m
+++ b/simulator/src/prints.m
@@ -67,9 +67,9 @@ maxTemperature = (externalTemp*(1+(((gamma-1)/2)*(mach(iMaxV)^2))))-273.15;
 % end
 
 % longitudinal XCPs
-lonXCPs = -ascent.coeff.XCPlon(~isnan(ascent.coeff.XCPlon));
-latXCPs = -ascent.coeff.XCPlat(~isnan(ascent.coeff.XCPlat));
-totXCPs = ascent.coeff.XCPtot(~isnan(ascent.coeff.XCPtot));
+% lonXCPs = -ascent.coeff.XCPlon(~isnan(ascent.coeff.XCPlon));
+% latXCPs = -ascent.coeff.XCPlat(~isnan(ascent.coeff.XCPlat));
+totXCPs = ascent.coeff.xcp(~isnan(ascent.coeff.xcp));
 
 % DATA RECORD (display)
 disp(' ')
@@ -101,7 +101,8 @@ 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', 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));
-- 
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