Merge pull request #266 from teyrana/testfix
2 Small fixes to address test suite failures
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commit
f2155f0e39
@ -26,7 +26,7 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
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protected boolean ignitionOveride = false;
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protected double ignitionDelay = 0.0;
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protected IgnitionEvent ignitionEvent = IgnitionEvent.NEVER;
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protected IgnitionEvent ignitionEvent = IgnitionEvent.AUTOMATIC;
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protected int modID = 0;
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@ -41,13 +41,7 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
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this.mount = _mount;
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this.fcid = _fcid;
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this.id = new MotorConfigurationId( _mount, _fcid );
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this.motor = null;
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ejectionDelay = 0.0;
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ignitionEvent = IgnitionEvent.NEVER;
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ignitionDelay = 0.0;
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modID++;
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}
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@ -81,7 +81,6 @@ public class BarrowmanCalculatorTest {
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exp_cpx = ( cna_nose*cpx_nose + cna_body*cpx_body + cna_3fin*cpx_3fin + cna_lugs*cpx_lugs)/exp_cna;
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}
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// calculated from OpenRocket 15.03
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Coordinate cp_calc = calc.getCP(config, conditions, warnings);
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assertEquals(" Estes Alpha III CNa value is incorrect:", exp_cna, cp_calc.weight, EPSILON);
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@ -117,9 +116,8 @@ public class BarrowmanCalculatorTest {
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FlightConditions conditions = new FlightConditions(config);
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WarningSet warnings = new WarningSet();
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// no clue:
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double expCPx = 1.0367644;
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double expCNa = 14.169;
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double expCPx = 0.994642;
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double expCNa = 15.437111;
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Coordinate calcCP = calc.getCP(config, conditions, warnings);
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assertEquals(" Falcon 9 Heavy CP x value is incorrect:", expCPx, calcCP.x, EPSILON);
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@ -29,6 +29,7 @@
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<exclude-output />
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<content url="file://$MODULE_DIR$">
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<sourceFolder url="file://$MODULE_DIR$/src" isTestSource="false" />
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<sourceFolder url="file://$MODULE_DIR$/test" isTestSource="true" />
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</content>
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<orderEntry type="sourceFolder" forTests="false" />
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<orderEntry type="inheritedJdk" />
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@ -206,5 +207,6 @@
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<SOURCES />
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</library>
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</orderEntry>
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<orderEntry type="library" name="junit-dep-4.8.2" level="project" />
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</component>
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</module>
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@ -28,17 +28,12 @@ import net.sf.openrocket.file.motor.GeneralMotorLoader;
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import net.sf.openrocket.gui.main.UndoRedoAction;
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import net.sf.openrocket.l10n.DebugTranslator;
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import net.sf.openrocket.l10n.Translator;
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import net.sf.openrocket.masscalc.BasicMassCalculator;
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import net.sf.openrocket.masscalc.MassCalculator;
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import net.sf.openrocket.masscalc.MassCalculator.MassCalcType;
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import net.sf.openrocket.motor.Motor;
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import net.sf.openrocket.motor.ThrustCurveMotor;
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import net.sf.openrocket.plugin.PluginModule;
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import net.sf.openrocket.rocketcomponent.Configuration;
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import net.sf.openrocket.rocketcomponent.EngineBlock;
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import net.sf.openrocket.rocketcomponent.MassComponent;
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import net.sf.openrocket.rocketcomponent.NoseCone;
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import net.sf.openrocket.rocketcomponent.RocketComponent;
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import net.sf.openrocket.rocketcomponent.*;
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import net.sf.openrocket.simulation.FlightDataType;
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import net.sf.openrocket.simulation.exception.SimulationException;
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import net.sf.openrocket.startup.Application;
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@ -71,8 +66,8 @@ public class IntegrationTest {
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private Action undoAction, redoAction;
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private AerodynamicCalculator aeroCalc = new BarrowmanCalculator();
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private MassCalculator massCalc = new BasicMassCalculator();
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private Configuration config;
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private MassCalculator massCalc = new MassCalculator();
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private FlightConfiguration config;
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private FlightConditions conditions;
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private String massComponentID = null;
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@ -113,7 +108,8 @@ public class IntegrationTest {
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undoAction = UndoRedoAction.newUndoAction(document);
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redoAction = UndoRedoAction.newRedoAction(document);
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config = document.getSimulation(0).getConfiguration();
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FlightConfigurationId fcid = document.getSimulation(0).getFlightConfigurationId();
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config = document.getRocket().getFlightConfiguration(fcid);
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conditions = new FlightConditions(config);
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// Test undo state
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