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0 mass should be an abort, not an exception

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This commit is contained in:
JoePfeiffer 2024-02-24 06:39:29 -07:00
parent 7f7e4018ad
commit b285de1c49
1 changed files with 2 additions and 1 deletions
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3
core/src/net/sf/openrocket/simulation/AbstractEulerStepper.java
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@ -4,6 +4,7 @@ import org.slf4j.Logger;
import org.slf4j.LoggerFactory; import org.slf4j.LoggerFactory;
import net.sf.openrocket.l10n.Translator; import net.sf.openrocket.l10n.Translator;
import net.sf.openrocket.logging.SimulationAbort;
import net.sf.openrocket.models.atmosphere.AtmosphericConditions; import net.sf.openrocket.models.atmosphere.AtmosphericConditions;
import net.sf.openrocket.rocketcomponent.InstanceMap; import net.sf.openrocket.rocketcomponent.InstanceMap;
import net.sf.openrocket.rocketcomponent.RecoveryDevice; import net.sf.openrocket.rocketcomponent.RecoveryDevice;
@ -55,7 +56,7 @@ public abstract class AbstractEulerStepper extends AbstractSimulationStepper {
final double mass = rocketMass + motorMass; final double mass = rocketMass + motorMass;
if (mass < MathUtil.EPSILON) { if (mass < MathUtil.EPSILON) {
throw new SimulationException(trans.get("SimulationStepper.error.totalMassZero")); status.abortSimulation(SimulationAbort.Cause.ACTIVE_MASS_ZERO);
} }
// Compute drag acceleration // Compute drag acceleration