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Co-authored-by: gPauls-TUHH <gerrit.pauls@tuhh.de>

aerodynamic_analysis/src/taw/tawCalculatePolarConfig.h

@@ -123,9 +123,9 @@ class tawCalculatePolarConfig{
 
     /* High lift calibration data */
     struct hl_polar_calibration_values {
-        double CL_max;          /**< maximum CL value which should be reached */
-        double delta_CD;        /**< Constant delta for drag calibration */
-        double factor_CD;       /**< Factor for drag calibration */
+        double CL_max = NAN;          /**< maximum CL value which should be reached */
+        double delta_CD = NAN;        /**< Constant delta for drag calibration */
+        double factor_CD = NAN;       /**< Factor for drag calibration */
     };
     std::unordered_map<std::string, hl_polar_calibration_values> hl_polar_calibration_data; /**< Container for storing all high lift polar calibration and correction values */