When determining worst-case CP, only consider cases where the CP's weight is non-zero
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				| @ -4,6 +4,7 @@ import java.util.Map; | ||||
| 
 | ||||
| import net.sf.openrocket.rocketcomponent.FlightConfiguration; | ||||
| import net.sf.openrocket.rocketcomponent.RocketComponent; | ||||
| import net.sf.openrocket.util.MathUtil; | ||||
| import net.sf.openrocket.util.Coordinate; | ||||
| 
 | ||||
| 
 | ||||
| @ -62,7 +63,7 @@ public abstract class AbstractAerodynamicCalculator implements AerodynamicCalcul | ||||
| 		for (int i = 0; i < DIVISIONS; i++) { | ||||
| 			cond.setTheta(2 * Math.PI * i / DIVISIONS); | ||||
| 			cp = getCP(configuration, cond, warnings); | ||||
| 			if (cp.x < worst.x) { | ||||
| 			if ((cp.weight > MathUtil.EPSILON) && (cp.x < worst.x)) { | ||||
| 				worst = cp; | ||||
| 				theta = cond.getTheta(); | ||||
| 			} | ||||
|  | ||||
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