Fixed bug where performance_assessment stalls due to aero returning a NaN as drag

Description

Fixed bug where performance_assessment stalls due to aero returning a NaN as drag

Related Issue(s)

• Closes #[feature issues]
• Fixes #[bug report issue]
• Resolves #[any other issues]

Other Changes

• [Mention refactoring, tests, etc.]

Screenshots/Logs

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Testing Instructions

1. [Step 1: How to test]
2. [Step 2: Expected outcome]
3. [Step 3: Additional steps if required]

Developer Checklist

• Code has been tested locally and/or in pipeline.
• (if applicable) documentation updated.
• (if applicable) impact of new dependencies reviewed and included in project.
• Merge conflicts resolved with the target branch.

Additional Notes

Add any information reviewers should focus on, e.g., specific files, functions, or changes of interest.

performance_assessment/src/taw/defaultMethods/aircraft.cpp

@@ -216,6 +216,9 @@ double aircraft::ROC(double Mass, double Alt, double Mach, double fACC, string C
     } catch (const std::string& e) {
         tempDrag = ac_thrust;  // In case of missing polar data a gamma of 0 is forced
     }
+    if (std::isnan(tempDrag)) {
+        tempDrag = ac_thrust;  // In case of missing polar data (but NaN-flavoured)
+    }
     double tempGamma = asin((ac_thrust - tempDrag) / (G_FORCE * Mass) / (1. + fACC));  // because not with const. TAS but with const. IAS or Ma is risen
                                                                                     //--> Introduction of facc: Commutation factor: facc = V/g * dV/dh; see table 11.1 p.232
     double tempLiftCoefficient = 2.*(G_FORCE * Mass * cos(tempGamma))