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Merge pull request #266 from teyrana/testfix

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2 Small fixes to address test suite failures
This commit is contained in:
kruland2607 2016-04-06 16:52:18 -05:00
commit f2155f0e39
4 changed files with 11 additions and 21 deletions
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8
core/src/net/sf/openrocket/motor/MotorConfiguration.java
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@ -26,7 +26,7 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
protected boolean ignitionOveride = false;
protected double ignitionDelay = 0.0;
protected IgnitionEvent ignitionEvent = IgnitionEvent.NEVER;
protected IgnitionEvent ignitionEvent = IgnitionEvent.AUTOMATIC;
protected int modID = 0;
@ -42,12 +42,6 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
this.fcid = _fcid;
this.id = new MotorConfigurationId( _mount, _fcid );
this.motor = null;
ejectionDelay = 0.0;
ignitionEvent = IgnitionEvent.NEVER;
ignitionDelay = 0.0;
modID++;
}

6
core/test/net/sf/openrocket/aerodynamics/BarrowmanCalculatorTest.java
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@ -81,7 +81,6 @@ public class BarrowmanCalculatorTest {
exp_cpx = ( cna_nose*cpx_nose + cna_body*cpx_body + cna_3fin*cpx_3fin + cna_lugs*cpx_lugs)/exp_cna;
}
// calculated from OpenRocket 15.03
Coordinate cp_calc = calc.getCP(config, conditions, warnings);
assertEquals(" Estes Alpha III CNa value is incorrect:", exp_cna, cp_calc.weight, EPSILON);
@ -117,9 +116,8 @@ public class BarrowmanCalculatorTest {
FlightConditions conditions = new FlightConditions(config);
WarningSet warnings = new WarningSet();
// no clue:
double expCPx = 1.0367644;
double expCNa = 14.169;
double expCPx = 0.994642;
double expCNa = 15.437111;
Coordinate calcCP = calc.getCP(config, conditions, warnings);
assertEquals(" Falcon 9 Heavy CP x value is incorrect:", expCPx, calcCP.x, EPSILON);

2
swing/OpenRocket Swing.iml
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@ -29,6 +29,7 @@
<exclude-output />
<content url="file://$MODULE_DIR$">
<sourceFolder url="file://$MODULE_DIR$/src" isTestSource="false" />
<sourceFolder url="file://$MODULE_DIR$/test" isTestSource="true" />
</content>
<orderEntry type="sourceFolder" forTests="false" />
<orderEntry type="inheritedJdk" />
@ -206,5 +207,6 @@
<SOURCES />
</library>
</orderEntry>
<orderEntry type="library" name="junit-dep-4.8.2" level="project" />
</component>
</module>

14
swing/test/net/sf/openrocket/IntegrationTest.java
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@ -28,17 +28,12 @@ import net.sf.openrocket.file.motor.GeneralMotorLoader;
import net.sf.openrocket.gui.main.UndoRedoAction;
import net.sf.openrocket.l10n.DebugTranslator;
import net.sf.openrocket.l10n.Translator;
import net.sf.openrocket.masscalc.BasicMassCalculator;
import net.sf.openrocket.masscalc.MassCalculator;
import net.sf.openrocket.masscalc.MassCalculator.MassCalcType;
import net.sf.openrocket.motor.Motor;
import net.sf.openrocket.motor.ThrustCurveMotor;
import net.sf.openrocket.plugin.PluginModule;
import net.sf.openrocket.rocketcomponent.Configuration;
import net.sf.openrocket.rocketcomponent.EngineBlock;
import net.sf.openrocket.rocketcomponent.MassComponent;
import net.sf.openrocket.rocketcomponent.NoseCone;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.*;
import net.sf.openrocket.simulation.FlightDataType;
import net.sf.openrocket.simulation.exception.SimulationException;
import net.sf.openrocket.startup.Application;
@ -71,8 +66,8 @@ public class IntegrationTest {
private Action undoAction, redoAction;
private AerodynamicCalculator aeroCalc = new BarrowmanCalculator();
private MassCalculator massCalc = new BasicMassCalculator();
private Configuration config;
private MassCalculator massCalc = new MassCalculator();
private FlightConfiguration config;
private FlightConditions conditions;
private String massComponentID = null;
@ -113,7 +108,8 @@ public class IntegrationTest {
undoAction = UndoRedoAction.newUndoAction(document);
redoAction = UndoRedoAction.newRedoAction(document);
config = document.getSimulation(0).getConfiguration();
FlightConfigurationId fcid = document.getSimulation(0).getFlightConfigurationId();
config = document.getRocket().getFlightConfiguration(fcid);
conditions = new FlightConditions(config);
// Test undo state