removed pkill from plot; added module specifier; fixed bug on plotOn flag

empennage_design/src/taw/conventional/low/lowConventionalEmpennageDesignPlot.cpp

@@ -133,11 +133,6 @@ fs::path Conventional::plot_stabilizer_planform(
     chordwise.push_back(it->origin.x() + it->get_chord_length());
   }
 
-  // /* Get mac coordinates */
-  // auto mac_position_y = geom2::measure::mean_aerodynamic_chord_position(data->wing);
-  // auto mac_position = geom2::measure::offset_LE(data->wing,mac_position_y);
-  // auto mac = geom2::measure::chord(data->wing,mac_position_y);
-
   /* Generate plot */
   std::string name = surface.name;
   std::replace(name.begin(), name.end(), '_', ' ');
@@ -203,17 +198,16 @@ fs::path Conventional::plot_stabilizer_planform(
   ax->legend()->box(true);
   ax->legend()->font_size(8);
 
-  fs::path plot_path = rtIO->getPlotDir() + "/" + surface.name + "_planfrom.svg";
+  fs::path plot_path = rtIO->getPlotDir() + "/empennage_design_" + surface.name + "_planform.svg";
   matplot::save(f, plot_path.string(), "svg");
   std::this_thread::sleep_for(std::chrono::milliseconds(500));
-  system("pkill gnuplot");
   return fs::relative(plot_path, fs::path(rtIO->getHtmlDir()));
 }
 
 fs::path Conventional::plot_thickness_and_twist_distribution(
     const geom2::MultisectionSurface<geom2::AirfoilSection>& surface) {
   /* Plot active */
-  if (rtIO->plotOn) {
+  if (!rtIO->plotOn) {
     return "";
   }
   std::vector<double> eta;
@@ -245,10 +239,9 @@ fs::path Conventional::plot_thickness_and_twist_distribution(
   ax2->grid(true);
   ax2->ylim({*twist_min - 0.01, *twist_max + 0.01});
 
-  fs::path plot_path = rtIO->getPlotDir() + "/" + surface.name + "_thickness_and_twist_distribution.svg";
+  fs::path plot_path = rtIO->getPlotDir() + "/empennage_design_" + surface.name + "_thickness_and_twist_distribution.svg";
   matplot::save(f, plot_path.string(), "svg");
   std::this_thread::sleep_for(std::chrono::milliseconds(500));
-  system("pkill gnuplot");
   return fs::relative(plot_path, fs::path(rtIO->getHtmlDir()));
 }
 
@@ -296,11 +289,10 @@ std::vector<fs::path> Conventional::plot_airfoils(const geom2::MultisectionSurfa
       ax->xlim({0, 1});
       ax->axis(matplot::equal);
 
-      fs::path plot_path = rtIO->getPlotDir() + "/" + surface.name + "_" + airfoil_data.first + "_airfoil.svg";
+      fs::path plot_path = rtIO->getPlotDir() + "/empennage_design_" + surface.name + "_" + airfoil_data.first + "_airfoil.svg";
       matplot::save(f, plot_path.string(), "svg");
       airfoil_plots_path.push_back(fs::relative(plot_path, fs::path(rtIO->getHtmlDir())));
       std::this_thread::sleep_for(std::chrono::milliseconds(500));
-      system("pkill gnuplot");
     }
   }
   return airfoil_plots_path;