applied sugestions regarding bwb config

aerodynamic_analysis/src/bwb/bwbCalculatePolarConfig.cpp

@@ -46,7 +46,7 @@ bwbCalculatePolarConfig::bwbCalculatePolarConfig(const node& config)
     pathToLiftingLine(EndnodeReadOnly<std::string>("program_settings/LiftingLine/FolderPath")),
     stepWidthCL(EndnodeReadOnly<double>("LiftingLineForTAW/stepWidthCL")),
     // other settings
-    setFlightConditionsMode(EndnodeReadOnly<std::string>("program_settings/FlightConditions/AdaptMachNumbersToCruiseReq")),
+    setFlightConditionsMode(EndnodeReadOnly<bool>("program_settings/FlightConditions/AdaptMachNumbersToCruiseReq").read(config).value()),
     // lifting line for TAW pitching moment corrections
     delta_CM0(EndnodeReadOnly<double>("LiftingLineForTAW/PitchingMoment/delta_CM0")),
     delta_dCMdCL(EndnodeReadOnly<double>("LiftingLineForTAW/PitchingMoment/delta_dCMdCL")),
@@ -80,7 +80,6 @@ bwbCalculatePolarConfig::bwbCalculatePolarConfig(const node& config)
     factorDragHL(EndnodeReadOnly<double>("program_settings/SemiEmpiricalHighLiftAdaptions/factorDrag")) {
     CLModeAirfoilSelection.read(config);
     stepWidthCL.read(config);
-    setFlightConditionsMode.read(config);
     pathToLiftingLine.read(config);
     manualTransition.read(config);
     manualTransitionWing.read(config);
@@ -110,13 +109,13 @@ bwbCalculatePolarConfig::bwbCalculatePolarConfig(const node& config)
     deltaTotalDragHL.read(config);
     factorDragHL.read(config);
     myRuntimeInfo->out << "config: " << liftingLineFolderPath << endl;
-    if (setFlightConditionsMode.value() == "mode_0") {
+    if (setFlightConditionsMode == false) {
         myRuntimeInfo->info << "set flight conditions from config xml" << endl;
         size_t numberFlightConditions(config.getVector(("program_settings/FlightConditions/FlightCondition"), 2).size());
         for (size_t i(0); i < numberFlightConditions; i++) {
             readFlightConditions(config, i);
         }
-    } else if (setFlightConditionsMode.value() == "mode_1") {
+    } else if (setFlightConditionsMode == true) {
         myRuntimeInfo->info << "Hab vergessen was hier rein sollte" << endl;
     }
     CGPositions = {"design", "forward", "aft"};

aerodynamic_analysis/src/bwb/bwbCalculatePolarConfig.h

@@ -43,7 +43,7 @@ class bwbCalculatePolarConfig{
     EndnodeReadOnly<std::string> CLModeAirfoilSelection;    /**< Switch which sets if lift coefficient at ICA, at TOC or at average cruise is chosen for airfoil selection */
     EndnodeReadOnly<double> stepWidthCL;
     // fligt condition parameters
-    EndnodeReadOnly<std::string> setFlightConditionsMode;
+    bool setFlightConditionsMode;
     // lifting line pitching moment parameters
     EndnodeReadOnly<double> delta_CM0;
     EndnodeReadOnly<double> delta_dCMdCL;