diff --git a/simulator/mainSimulator.m b/simulator/mainSimulator.m index b9ec897857d6eae5de45f3019d59db52b87435f9..39d184ab2587fe9ddfafb7a3c95a67adc1b6d0d0 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 599b37c96e1002df1624277378889a29731d9757..38bacbf0b5e0666bdc4d6dd25d248569c46c6ea9 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));