Merge branch 'unstable' into issue-1791

This commit is contained in:
SiboVG 2022-11-10 00:40:20 +01:00
commit 4691bb2ae3
27 changed files with 2007 additions and 79 deletions

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@ -140,12 +140,11 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
WarningSet warnings)
{
// forces for this component, and all forces below it, in the rocket-tree
// => regardless `if(comp isinstance ComponentAssembly)`, or not.
AerodynamicForces aggregateForces = new AerodynamicForces().zero();
aggregateForces.setComponent(comp);
// forces for this component, _only_
if(comp.isAerodynamic()) {
if(comp.isAerodynamic() || comp instanceof ComponentAssembly) {
RocketComponentCalc calcObj = calcMap.get(comp);
if (null == calcObj) {
throw new NullPointerException("Could not find a CalculationObject for aerodynamic Component!: " + comp.getComponentName());
@ -163,6 +162,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
if (child instanceof AxialStage && !configuration.isStageActive(child.getStageNumber())) {
continue;
}
// forces particular to each component
AerodynamicForces childForces = calculateForceAnalysis(configuration, conds, child, instances, eachForces, assemblyForces, warnings);
@ -173,7 +173,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
assemblyForces.put(comp, aggregateForces);
return eachForces.get(comp);
return assemblyForces.get(comp);
}
@Override
@ -944,7 +944,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
calcMap = new HashMap<>();
for (RocketComponent comp: configuration.getAllComponents()) {
if (!comp.isAerodynamic()) {
if (!comp.isAerodynamic() && !(comp instanceof ComponentAssembly)) {
continue;
}

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@ -0,0 +1,37 @@
package net.sf.openrocket.aerodynamics.barrowman;
import net.sf.openrocket.aerodynamics.AerodynamicForces;
import net.sf.openrocket.aerodynamics.FlightConditions;
import net.sf.openrocket.aerodynamics.WarningSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.util.Transformation;
/*
* Aerodynamic properties of a component assembly. Since an "assembly"
* has no impact except as a summation of its subparts, just returns 0
*
*/
public class ComponentAssemblyCalc extends RocketComponentCalc {
public ComponentAssemblyCalc(RocketComponent c) {
super(c);
}
@Override
public void calculateNonaxialForces(FlightConditions conditions, Transformation transform,
AerodynamicForces forces, WarningSet warnings) {
// empty
}
@Override
public double calculateFrictionCD(FlightConditions conditions, double componentCf, WarningSet warnings) {
return 0;
}
@Override
public double calculatePressureCD(FlightConditions conditions,
double stagnationCD, double baseCD, WarningSet warnings) {
return 0;
}
}

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@ -308,7 +308,7 @@ public class Simulation implements ChangeSource, Cloneable {
*/
public Status getStatus() {
mutex.verify();
if (status == Status.UPTODATE || status == Status.LOADED) {
if (isStatusUpToDate(status)) {
if (rocket.getFunctionalModID() != simulatedRocketID || !options.equals(simulatedConditions)) {
status = Status.OUTDATED;
}
@ -330,6 +330,14 @@ public class Simulation implements ChangeSource, Cloneable {
return status;
}
/**
* Returns true is the status indicates that the simulation data is up-to-date.
* @param status status of the simulation to check for if its data is up-to-date
*/
public static boolean isStatusUpToDate(Status status) {
return status == Status.UPTODATE || status == Status.LOADED || status == Status.EXTERNAL;
}

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@ -29,6 +29,8 @@ public class RockSimCommonConstants {
public static final String DENSITY_TYPE = "DensityType";
public static final String RADIAL_LOC = "RadialLoc";
public static final String RADIAL_ANGLE = "RadialAngle";
public static final String AUTO_CALC_RADIAL_DISTANCE = "AutoCalcRadialDistance";
public static final String AUTO_CALC_RADIAL_ANGLE = "AutoCalcRadialAngle";
public static final String LOCATION_MODE = "LocationMode";
public static final String FINISH_CODE = "FinishCode";
public static final String SERIAL_NUMBER = "SerialNo";

View File

@ -11,6 +11,7 @@ import net.sf.openrocket.rocketcomponent.InnerTube;
import net.sf.openrocket.rocketcomponent.LaunchLug;
import net.sf.openrocket.rocketcomponent.MassObject;
import net.sf.openrocket.rocketcomponent.Parachute;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.Streamer;
import net.sf.openrocket.rocketcomponent.Transition;
@ -50,6 +51,7 @@ public class BodyTubeDTO extends BasePartDTO implements AttachableParts {
@XmlElementRefs({
@XmlElementRef(name = RockSimCommonConstants.BODY_TUBE, type = BodyTubeDTO.class),
@XmlElementRef(name = RockSimCommonConstants.BODY_TUBE, type = InnerBodyTubeDTO.class),
@XmlElementRef(name = RockSimCommonConstants.TRANSITION, type = TransitionDTO.class),
@XmlElementRef(name = RockSimCommonConstants.RING, type = CenteringRingDTO.class),
@XmlElementRef(name = RockSimCommonConstants.LAUNCH_LUG, type = LaunchLugDTO.class),
@XmlElementRef(name = RockSimCommonConstants.FIN_SET, type = FinSetDTO.class),
@ -57,7 +59,8 @@ public class BodyTubeDTO extends BasePartDTO implements AttachableParts {
@XmlElementRef(name = RockSimCommonConstants.TUBE_FIN_SET, type = TubeFinSetDTO.class),
@XmlElementRef(name = RockSimCommonConstants.STREAMER, type = StreamerDTO.class),
@XmlElementRef(name = RockSimCommonConstants.PARACHUTE, type = ParachuteDTO.class),
@XmlElementRef(name = RockSimCommonConstants.MASS_OBJECT, type = MassObjectDTO.class)})
@XmlElementRef(name = RockSimCommonConstants.MASS_OBJECT, type = MassObjectDTO.class),
@XmlElementRef(name = RockSimCommonConstants.EXTERNAL_POD, type = PodSetDTO.class)})
List<BasePartDTO> attachedParts = new ArrayList<BasePartDTO>();
/**
@ -125,6 +128,8 @@ public class BodyTubeDTO extends BasePartDTO implements AttachableParts {
addAttachedPart(new FinSetDTO((FinSet) rocketComponents));
} else if (rocketComponents instanceof TubeFinSet) {
addAttachedPart(new TubeFinSetDTO((TubeFinSet) rocketComponents));
} else if (rocketComponents instanceof PodSet) {
addAttachedPart(new PodSetDTO((PodSet) rocketComponents));
}
}
}

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@ -0,0 +1,110 @@
package net.sf.openrocket.file.rocksim.export;
import net.sf.openrocket.file.rocksim.RockSimCommonConstants;
import net.sf.openrocket.rocketcomponent.BodyTube;
import net.sf.openrocket.rocketcomponent.NoseCone;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.Transition;
import net.sf.openrocket.rocketcomponent.position.AxialMethod;
import net.sf.openrocket.rocketcomponent.position.RadiusMethod;
import javax.xml.bind.annotation.XmlAccessType;
import javax.xml.bind.annotation.XmlAccessorType;
import javax.xml.bind.annotation.XmlElement;
import javax.xml.bind.annotation.XmlElementRef;
import javax.xml.bind.annotation.XmlElementRefs;
import javax.xml.bind.annotation.XmlElementWrapper;
import javax.xml.bind.annotation.XmlRootElement;
import java.util.ArrayList;
import java.util.List;
/**
* Models the XML element for a RockSim pod.
*/
@XmlRootElement(name = RockSimCommonConstants.EXTERNAL_POD)
@XmlAccessorType(XmlAccessType.FIELD)
public class PodSetDTO extends BasePartDTO implements AttachableParts {
@XmlElement(name = RockSimCommonConstants.AUTO_CALC_RADIAL_DISTANCE)
private int autoCalcRadialDistance = 0;
@XmlElement(name = RockSimCommonConstants.AUTO_CALC_RADIAL_ANGLE)
private int autoCalcRadialAngle = 0;
@XmlElementWrapper(name = RockSimCommonConstants.ATTACHED_PARTS)
@XmlElementRefs({
@XmlElementRef(name = RockSimCommonConstants.BODY_TUBE, type = BodyTubeDTO.class),
@XmlElementRef(name = RockSimCommonConstants.NOSE_CONE, type = NoseConeDTO.class),
@XmlElementRef(name = RockSimCommonConstants.TRANSITION, type = TransitionDTO.class),
@XmlElementRef(name = RockSimCommonConstants.EXTERNAL_POD, type = PodSetDTO.class)})
List<BasePartDTO> attachedParts = new ArrayList<BasePartDTO>();
/**
* Default constructor.
*/
public PodSetDTO() {
}
/**
* Copy constructor. Fully populates this instance with values taken from the OR PodSet.
*
* @param theORPodSet
*/
public PodSetDTO(PodSet theORPodSet) {
super(theORPodSet);
// OR should always override the radial angle and distance
setAutoCalcRadialDistance(false);
setAutoCalcRadialAngle(false);
setRadialAngle(theORPodSet.getAngleOffset());
setRadialLoc(theORPodSet.getRadiusMethod().getRadius(
theORPodSet.getParent(), theORPodSet,
theORPodSet.getRadiusOffset()) * RockSimCommonConstants.ROCKSIM_TO_OPENROCKET_LENGTH);
setXb(theORPodSet.getAxialOffset(AxialMethod.TOP) * RockSimCommonConstants.ROCKSIM_TO_OPENROCKET_LENGTH);
for (RocketComponent child : theORPodSet.getChildren()) {
if (child instanceof PodSet) {
addAttachedPart(new PodSetDTO((PodSet) child));
} else if (child instanceof BodyTube) {
addAttachedPart(new BodyTubeDTO((BodyTube) child));
} else if (child instanceof NoseCone) {
addAttachedPart(new NoseConeDTO((NoseCone) child));
} else if (child instanceof Transition) {
addAttachedPart(new TransitionDTO((Transition) child));
}
}
}
public int getAutoCalcRadialDistance() {
return autoCalcRadialDistance;
}
public void setAutoCalcRadialDistance(boolean motorMount) {
if (motorMount) {
this.autoCalcRadialDistance = 1;
} else {
this.autoCalcRadialDistance = 0;
}
}
public int getAutoCalcRadialAngle() {
return autoCalcRadialAngle;
}
public void setAutoCalcRadialAngle(boolean motorMount) {
if (motorMount) {
this.autoCalcRadialAngle = 1;
} else {
this.autoCalcRadialAngle = 0;
}
}
@Override
public void addAttachedPart(BasePartDTO part) {
if (!attachedParts.contains(part)) {
attachedParts.add(part);
}
}
@Override
public void removeAttachedPart(BasePartDTO part) {
attachedParts.remove(part);
}
}

View File

@ -8,6 +8,7 @@ import net.sf.openrocket.file.DocumentLoadingContext;
import net.sf.openrocket.file.rocksim.RockSimCommonConstants;
import net.sf.openrocket.file.simplesax.AbstractElementHandler;
import net.sf.openrocket.file.simplesax.ElementHandler;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import java.util.HashMap;
@ -68,23 +69,32 @@ class AttachedPartsHandler extends AbstractElementHandler {
return new RingHandler(context, component, warnings);
}
if (RockSimCommonConstants.BODY_TUBE.equals(element)) {
return new InnerBodyTubeHandler(context, component, warnings);
// Pods can have BodyTubes as attached parts, but not inner tubes. All other components can't have BodyTubes as
// attached parts.
if (component instanceof PodSet) {
return new BodyTubeHandler(context, component, warnings);
} else {
return new InnerBodyTubeHandler(context, component, warnings);
}
}
if (RockSimCommonConstants.TRANSITION.equals(element)) {
return new TransitionHandler(context, component, warnings);
}
if (RockSimCommonConstants.NOSE_CONE.equals(element)) {
return new NoseConeHandler(context, component, warnings);
}
if (RockSimCommonConstants.SUBASSEMBLY.equals(element)) {
return new SubAssemblyHandler(context, component);
}
if (RockSimCommonConstants.TUBE_FIN_SET.equals(element)) {
return new TubeFinSetHandler(context, component, warnings);
}
if (RockSimCommonConstants.EXTERNAL_POD.equals(element)) {
return new PodHandler(context, component, warnings);
}
if (RockSimCommonConstants.RING_TAIL.equals(element)) {
warnings.add("Ring tails are not currently supported. Ignoring.");
}
if (RockSimCommonConstants.EXTERNAL_POD.equals(element)) {
warnings.add("Pods are not currently supported. Ignoring.");
}
return null;
}
}

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@ -25,6 +25,7 @@ class BodyTubeHandler extends BaseHandler<BodyTube> {
* The OpenRocket BodyTube.
*/
private final BodyTube bodyTube;
private int isInsideTube = 0;
/**
* Constructor.
@ -80,6 +81,9 @@ class BodyTubeHandler extends BaseHandler<BodyTube> {
if (RockSimCommonConstants.MATERIAL.equals(element)) {
setMaterialName(content);
}
if (RockSimCommonConstants.IS_INSIDE_TUBE.equals(element)) {
isInsideTube = Integer.parseInt(content);
}
} catch (NumberFormatException nfe) {
warnings.add("Could not convert " + element + " value of " + content + ". It is expected to be a number.");
}
@ -104,4 +108,11 @@ class BodyTubeHandler extends BaseHandler<BodyTube> {
public Material.Type getMaterialType() {
return Material.Type.BULK;
}
/**
* Returns 0 if this is a body tube, 1 if it is an inside tube.
*/
public int isInsideTube() {
return isInsideTube;
}
}

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@ -0,0 +1,66 @@
package net.sf.openrocket.file.rocksim.importt;
import net.sf.openrocket.aerodynamics.WarningSet;
import net.sf.openrocket.file.DocumentLoadingContext;
import net.sf.openrocket.file.rocksim.RockSimCommonConstants;
import net.sf.openrocket.file.simplesax.ElementHandler;
import net.sf.openrocket.file.simplesax.PlainTextHandler;
import net.sf.openrocket.material.Material;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.position.RadiusMethod;
import org.xml.sax.SAXException;
import java.util.HashMap;
public class PodHandler extends PositionDependentHandler<PodSet> {
/**
* The OpenRocket BodyTube.
*/
private final PodSet podSet;
public PodHandler(DocumentLoadingContext context, RocketComponent c, WarningSet warnings) {
super(context);
if (c == null) {
throw new IllegalArgumentException("The parent component of a pod set may not be null.");
}
podSet = new PodSet();
podSet.setInstanceCount(1); // RockSim only supports one pod instance
podSet.setRadiusMethod(RadiusMethod.FREE); // RockSim radial offset is relative to the center of the parent
if (isCompatible(c, PodSet.class, warnings)) {
c.addChild(podSet);
}
}
@Override
public ElementHandler openElement(String element, HashMap<String, String> attributes, WarningSet warnings) throws SAXException {
if (RockSimCommonConstants.BODY_TUBE.equals(element)) { // RockSim pods allow body tubes, not inner tubes
return new BodyTubeHandler(context, podSet, warnings);
}
if (RockSimCommonConstants.ATTACHED_PARTS.equals(element)) {
return new AttachedPartsHandler(context, podSet);
}
return PlainTextHandler.INSTANCE;
}
@Override
public void closeElement(String element, HashMap<String, String> attributes, String content, WarningSet warnings) throws SAXException {
super.closeElement(element, attributes, content, warnings);
if (RockSimCommonConstants.RADIAL_ANGLE.equals(element)) {
podSet.setAngleOffset(Double.parseDouble(content));
}
if (RockSimCommonConstants.RADIAL_LOC.equals(element)) {
podSet.setRadiusOffset(Double.parseDouble(content) / RockSimCommonConstants.ROCKSIM_TO_OPENROCKET_LENGTH);
}
}
@Override
protected PodSet getComponent() {
return podSet;
}
@Override
protected Material.Type getMaterialType() {
return Material.Type.BULK;
}
}

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@ -9,6 +9,8 @@ import net.sf.openrocket.aerodynamics.WarningSet;
import net.sf.openrocket.file.DocumentLoadingContext;
import net.sf.openrocket.file.rocksim.RockSimCommonConstants;
import net.sf.openrocket.file.rocksim.RockSimLocationMode;
import net.sf.openrocket.rocketcomponent.ComponentAssembly;
import net.sf.openrocket.rocketcomponent.ParallelStage;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.position.AxialMethod;
@ -70,6 +72,10 @@ public abstract class PositionDependentHandler<C extends RocketComponent> extend
* Set the axialMethod of a component.
*/
protected void setLocation() {
if ((getComponent() instanceof ComponentAssembly || getComponent() instanceof ParallelStage) &&
getComponent().getParent() == null) {
return;
}
getComponent().setAxialMethod(axialMethod);
if (axialMethod.equals(AxialMethod.BOTTOM)) {
getComponent().setAxialOffset(-1d * positionValue);

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@ -121,19 +121,23 @@ public class PodSet extends ComponentAssembly implements RingInstanceable {
@Override
public double getAxialOffset() {
return getAxialOffset(this.axialMethod);
}
@Override
public double getAxialOffset(AxialMethod method) {
double returnValue;
if (this.isAfter()){
// remember the implicit (this instanceof Stage)
throw new BugException("found a pod positioned via: AFTER, but is not on the centerline?!: " + this.getName() + " is " + this.getAxialMethod().name() );
} else {
returnValue = super.getAxialOffset(this.axialMethod);
returnValue = super.getAxialOffset(method);
}
if (MathUtil.EPSILON > Math.abs(returnValue)) {
returnValue = 0.0;
}
return returnValue;
}

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@ -221,25 +221,16 @@ public class BasicEventSimulationEngine implements SimulationEngine {
// and thrust < THRUST_TUMBLE_CONDITION threshold
if (!currentStatus.isTumbling()) {
final double t = currentStatus.getFlightData().getLast(FlightDataType.TYPE_THRUST_FORCE);
final double cp = currentStatus.getFlightData().getLast(FlightDataType.TYPE_CP_LOCATION);
final double cg = currentStatus.getFlightData().getLast(FlightDataType.TYPE_CG_LOCATION);
final double aoa = currentStatus.getFlightData().getLast(FlightDataType.TYPE_AOA);
final boolean wantToTumble = (cg > cp && aoa > AOA_TUMBLE_CONDITION);
if (wantToTumble) {
final boolean tooMuchThrust = t > THRUST_TUMBLE_CONDITION;
final boolean isSustainer = currentStatus.getConfiguration().isStageActive(0);
final boolean isApogee = currentStatus.isApogeeReached();
if (tooMuchThrust) {
currentStatus.getWarnings().add(Warning.TUMBLE_UNDER_THRUST);
} else if (isApogee || !isSustainer) {
addEvent(new FlightEvent(FlightEvent.Type.TUMBLE, currentStatus.getSimulationTime()));
currentStatus.setTumbling(true);
}
}
final boolean isSustainer = currentStatus.getConfiguration().isStageActive(0);
final boolean isApogee = currentStatus.isApogeeReached();
if (wantToTumble && (isApogee || !isSustainer)) {
addEvent(new FlightEvent(FlightEvent.Type.TUMBLE, currentStatus.getSimulationTime()));
}
}
// If I'm on the ground and have no events in the queue, I'm done
@ -535,6 +526,7 @@ public class BasicEventSimulationEngine implements SimulationEngine {
currentStatus.getFlightData().addEvent(event);
}
log.debug("deployed recovery devices: " + currentStatus.getDeployedRecoveryDevices().size() );
break;
case GROUND_HIT:
@ -556,10 +548,19 @@ public class BasicEventSimulationEngine implements SimulationEngine {
break;
case TUMBLE:
if (!currentStatus.isLanded()) {
currentStepper = tumbleStepper;
currentStatus = currentStepper.initialize(currentStatus);
}
// Inhibit if we've deployed a parachute or we're on the ground
if ((currentStatus.getDeployedRecoveryDevices().size() > 0) || currentStatus.isLanded())
break;
currentStepper = tumbleStepper;
currentStatus = currentStepper.initialize(currentStatus);
final boolean tooMuchThrust = currentStatus.getFlightData().getLast(FlightDataType.TYPE_THRUST_FORCE) > THRUST_TUMBLE_CONDITION;
if (tooMuchThrust) {
currentStatus.getWarnings().add(Warning.TUMBLE_UNDER_THRUST);
}
currentStatus.setTumbling(true);
currentStatus.getFlightData().addEvent(event);
break;
}

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@ -146,15 +146,33 @@ public class FlightEvent implements Comparable<FlightEvent> {
/**
* Compares this event to another event depending on the event time. Secondary
* sorting is performed on stages; lower (numerically higher) stage first. Tertiary
* sorting is performed based on the event type ordinal.
*/
@Override
public int compareTo(FlightEvent o) {
// first, sort on time
if (this.time < o.time)
return -1;
if (this.time > o.time)
return 1;
// second, sort on stage presence. Events with no source go first
if ((this.getSource() == null) && (o.getSource() != null))
return -1;
if ((this.getSource() != null) && (o.getSource() == null))
return 1;
// third, sort on stage order. Bigger stage number goes first
if ((this.getSource() != null) && (o.getSource() != null)) {
if (this.getSource().getStageNumber() > o.getSource().getStageNumber())
return -1;
if (this.getSource().getStageNumber() < o.getSource().getStageNumber())
return 1;
}
// finally, sort on event type
return this.type.ordinal() - o.type.ordinal();
}

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@ -217,7 +217,7 @@ public class TestRockets {
.setDiameter(0.029)
.setLength(0.124)
.setTimePoints(new double[] { 0, 1, 2 })
.setThrustPoints(new double[] { 0, 1, 0 })
.setThrustPoints(new double[] { 0, 20, 0 })
.setCGPoints(new Coordinate[] {
new Coordinate(.062, 0, 0, 0.123),new Coordinate(.062, 0, 0, .0935),new Coordinate(.062, 0, 0, 0.064)})
.setDigest("digest G77 test")

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@ -31,11 +31,14 @@ import net.sf.openrocket.rocketcomponent.InnerTube;
import net.sf.openrocket.rocketcomponent.MassComponent;
import net.sf.openrocket.rocketcomponent.NoseCone;
import net.sf.openrocket.rocketcomponent.Parachute;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.Rocket;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.ShockCord;
import net.sf.openrocket.rocketcomponent.Streamer;
import net.sf.openrocket.rocketcomponent.TubeCoupler;
import net.sf.openrocket.rocketcomponent.position.AxialMethod;
import net.sf.openrocket.rocketcomponent.position.RadiusMethod;
import org.junit.Assert;
import static org.junit.Assert.assertEquals;
import org.junit.Test;
@ -94,6 +97,72 @@ public class RockSimDocumentDTOTest extends RockSimTestBase {
output.delete();
}
/**
* Tests exporting a rocket with pods, and whether importing that same file results in the same pod configuration.
*/
@Test
public void testPodsExport() throws Exception {
OpenRocketDocument originalDocument = makePodsRocket();
Rocket originalRocket = originalDocument.getRocket();
// Convert to RockSim XML
String result = new RockSimSaver().marshalToRockSim(originalDocument);
// Write to .rkt file
Path output = Files.createTempFile("podsRocket", ".rkt");
Files.write(output, result.getBytes(StandardCharsets.UTF_8));
// Read the file
RockSimLoader loader = new RockSimLoader();
InputStream stream = new FileInputStream(output.toFile());
Assert.assertNotNull("Could not open podsRocket.rkt", stream);
OpenRocketDocument importedDocument = OpenRocketDocumentFactory.createEmptyRocket();
DocumentLoadingContext context = new DocumentLoadingContext();
context.setOpenRocketDocument(importedDocument);
context.setMotorFinder(new DatabaseMotorFinder());
loader.loadFromStream(context, new BufferedInputStream(stream));
Rocket importedRocket = importedDocument.getRocket();
// Test children counts
List<RocketComponent> originalChildren = originalRocket.getAllChildren();
List<RocketComponent> importedChildren = importedRocket.getAllChildren();
assertEquals(" Number of total children doesn't match",
originalChildren.size(), importedChildren.size());
assertEquals(" Number of rocket children doesn't match", 1, importedRocket.getChildCount());
AxialStage stage = (AxialStage) importedRocket.getChild(0);
assertEquals(" Number of stage children doesn't match", 2, stage.getChildCount());
BodyTube tube = (BodyTube) stage.getChild(1);
assertEquals(" Number of body tube children doesn't match", 3, tube.getChildCount());
PodSet pod1 = (PodSet) tube.getChild(0);
assertEquals(" Number of pod 1 children doesn't match", 1, pod1.getChildCount());
PodSet pod2 = (PodSet) tube.getChild(1);
assertEquals(" Number of pod 2 children doesn't match", 2, pod2.getChildCount());
PodSet pod3 = (PodSet) tube.getChild(2);
assertEquals(" Number of pod 3 children doesn't match", 0, pod3.getChildCount());
// Test component names
for (int i = 1; i < originalChildren.size(); i++) {
assertEquals(" Child " + i + " does not match",
originalChildren.get(i).getName(), importedChildren.get(i).getName());
}
// Test pod parameters
assertEquals(-0.14, pod1.getAxialOffset(), 0.0001);
assertEquals(0.065, pod1.getRadiusOffset(), 0.0001);
assertEquals(Math.PI, pod1.getAngleOffset(), 0.0001);
assertEquals(1, pod1.getInstanceCount());
assertEquals(0.02, pod2.getAxialOffset(), 0.0001);
assertEquals(0.025, pod2.getRadiusOffset(), 0.0001);
assertEquals(- Math.PI / 2, pod2.getAngleOffset(), 0.0001);
assertEquals(1, pod2.getInstanceCount());
assertEquals(0.23, pod3.getAxialOffset(), 0.0001);
assertEquals(0.06, pod3.getRadiusOffset(), 0.0001);
assertEquals(Math.PI / 3, pod3.getAngleOffset(), 0.0001);
assertEquals(1, pod3.getInstanceCount());
stream.close();
Files.delete(output);
}
/**
* Tests exporting a design where a tube coupler has children, which is not supported by RockSim, so the children
* need to be moved outside the tube coupler.
@ -142,19 +211,91 @@ public class RockSimDocumentDTOTest extends RockSimTestBase {
Files.delete(output);
}
private OpenRocketDocument makeTubeCouplerRocket() {
private OpenRocketDocument makePodsRocket() {
OpenRocketDocument document = OpenRocketDocumentFactory.createNewRocket();
Rocket rocket = document.getRocket();
AxialStage stage = rocket.getStage(0);
// Stage children
NoseCone noseCone = new NoseCone();
noseCone.setName("Nose Cone");
stage.addChild(noseCone);
BodyTube tube = new BodyTube();
tube.setName("Body Tube");
stage.addChild(tube);
// Body tube children
PodSet pod1 = new PodSet();
pod1.setName("Pod 1");
tube.addChild(pod1);
PodSet pod2 = new PodSet();
pod2.setName("Pod 2");
tube.addChild(pod2);
PodSet pod3 = new PodSet();
pod2.setName("Pod 3");
tube.addChild(pod3);
// Pod 1 children
NoseCone noseCone1 = new NoseCone();
noseCone1.setName("Nose Cone 1");
pod1.addChild(noseCone1);
// Pod 2 children
NoseCone noseCone2 = new NoseCone();
noseCone2.setName("Nose Cone 2");
pod2.addChild(noseCone2);
BodyTube tube2 = new BodyTube();
tube2.setName("Body Tube 2");
pod2.addChild(tube2);
// Set pod parameters
pod1.setInstanceCount(1);
pod2.setInstanceCount(2);
pod3.setInstanceCount(3);
pod1.setAxialMethod(AxialMethod.ABSOLUTE);
pod1.setAxialOffset(0.01);
pod2.setAxialMethod(AxialMethod.TOP);
pod2.setAxialOffset(0.02);
pod3.setAxialMethod(AxialMethod.BOTTOM);
pod3.setAxialOffset(0.03);
pod1.setRadiusMethod(RadiusMethod.RELATIVE);
pod1.setRadiusOffset(0.015);
pod2.setRadiusMethod(RadiusMethod.FREE);
pod2.setRadiusOffset(0.025);
pod3.setRadiusMethod(RadiusMethod.RELATIVE);
pod3.setRadiusOffset(0.035);
pod1.setAngleOffset(Math.PI);
pod2.setAngleOffset(- Math.PI / 2);
pod3.setAngleOffset(Math.PI / 3);
return document;
}
private OpenRocketDocument makeTubeCouplerRocket() {
OpenRocketDocument document = OpenRocketDocumentFactory.createNewRocket();
Rocket rocket = document.getRocket();
AxialStage stage = rocket.getStage(0);
// Stage children
NoseCone noseCone = new NoseCone();
noseCone.setName("Nose Cone");
stage.addChild(noseCone);
BodyTube tube = new BodyTube();
tube.setName("Body Tube");
stage.addChild(tube);
// Body tube children
TubeCoupler coupler = new TubeCoupler();
coupler.setName("Tube coupler 1");
tube.addChild(coupler);
TubeCoupler coupler3 = new TubeCoupler();
coupler3.setName("Tube Coupler 3");
tube.addChild(coupler3);
// Tube coupler 1 children
InnerTube innerTube = new InnerTube();
innerTube.setName("Inner Tube");
coupler.addChild(innerTube);
@ -182,9 +323,8 @@ public class RockSimDocumentDTOTest extends RockSimTestBase {
MassComponent massComponent = new MassComponent();
massComponent.setName("Mass Component");
coupler.addChild(massComponent);
TubeCoupler coupler3 = new TubeCoupler();
coupler3.setName("Tube Coupler 3");
tube.addChild(coupler3);
// Tube coupler 3 children
Parachute parachute2 = new Parachute();
parachute2.setName("Parachute 2");
coupler3.addChild(parachute2);

File diff suppressed because it is too large Load Diff

View File

@ -8,10 +8,17 @@ import java.io.BufferedInputStream;
import java.io.IOException;
import java.io.InputStream;
import net.sf.openrocket.rocketcomponent.Bulkhead;
import net.sf.openrocket.rocketcomponent.CenteringRing;
import net.sf.openrocket.rocketcomponent.FreeformFinSet;
import net.sf.openrocket.rocketcomponent.InnerTube;
import net.sf.openrocket.rocketcomponent.MassComponent;
import net.sf.openrocket.rocketcomponent.NoseCone;
import net.sf.openrocket.rocketcomponent.Parachute;
import net.sf.openrocket.rocketcomponent.PodSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.Transition;
import net.sf.openrocket.rocketcomponent.TrapezoidFinSet;
import net.sf.openrocket.util.Coordinate;
import net.sf.openrocket.util.MathUtil;
import org.junit.Assert;
@ -212,7 +219,41 @@ public class RockSimLoaderTest extends BaseTestCase {
Assert.assertEquals(0.185d, stage1.getOverrideMass(), 0.001);
Assert.assertTrue(stage1.isCGOverridden());
Assert.assertEquals(0.3d, stage1.getOverrideCG().x, 0.001);
Assert.assertEquals(3, loader.getWarnings().size());
Assert.assertEquals(2, loader.getWarnings().size());
NoseCone nc = (NoseCone) stage1.getChild(0);
Assert.assertEquals(2, nc.getChildCount());
Assert.assertEquals("Clay", nc.getChild(0).getName());
RocketComponent it = nc.getChild(1);
Assert.assertEquals(InnerTube.class, it.getClass());
Assert.assertEquals("Attachment Rod", it.getName());
Assert.assertEquals(3, it.getChildCount());
RocketComponent c = it.getChild(0);
Assert.assertEquals(CenteringRing.class, c.getClass());
Assert.assertEquals("Plate", c.getName());
c = it.getChild(1);
Assert.assertEquals(CenteringRing.class, c.getClass());
Assert.assertEquals("Sleeve ", c.getName());
c = it.getChild(2);
Assert.assertEquals(Parachute.class, c.getClass());
Assert.assertEquals("Nose Cone Parachute", c.getName());
BodyTube bt1 = (BodyTube) stage1.getChild(1);
Assert.assertEquals(5, bt1.getChildCount());
Assert.assertEquals("Centering ring", bt1.getChild(0).getName());
Assert.assertEquals("Centering ring", bt1.getChild(1).getName());
c = bt1.getChild(2);
Assert.assertEquals(InnerTube.class, c.getClass());
Assert.assertEquals("Body tube", c.getName());
Assert.assertEquals("Launch lug", bt1.getChild(3).getName());
Assert.assertEquals("Pod", bt1.getChild(4).getName());
PodSet pod = (PodSet) bt1.getChild(4);
Assert.assertEquals(1, pod.getChildCount());
c = pod.getChild(0);
Assert.assertEquals(BodyTube.class, c.getClass());
Assert.assertEquals("Body tube", pod.getChild(0).getName());
Assert.assertEquals(1, stage2.getChildCount());
Assert.assertEquals("2nd Stage Tube", stage2.getChild(0).getName());
@ -221,8 +262,8 @@ public class RockSimLoaderTest extends BaseTestCase {
Assert.assertTrue(stage2.isCGOverridden());
Assert.assertEquals(0.4d, stage2.getOverrideCG().x, 0.001);
BodyTube bt = (BodyTube) stage2.getChild(0);
LaunchLug ll = (LaunchLug) bt.getChild(6);
BodyTube bt2 = (BodyTube) stage2.getChild(0);
LaunchLug ll = (LaunchLug) bt2.getChild(6);
Assert.assertEquals(1.22d, ll.getAngleOffset(), 0.001);
Assert.assertEquals(2, stage3.getChildCount());
@ -342,6 +383,97 @@ public class RockSimLoaderTest extends BaseTestCase {
Assert.assertEquals(0, bodyTube3.getChildCount());
}
@Test
public void testPodRocket() throws IOException, RocketLoadException{
RockSimLoader loader = new RockSimLoader();
OpenRocketDocument doc = loadRockSimRocket(loader, "PodTest.rkt");
Assert.assertNotNull(doc);
Rocket rocket = doc.getRocket();
Assert.assertNotNull(rocket);
Assert.assertEquals("Pod Test", doc.getRocket().getName());
Assert.assertEquals(3, loader.getWarnings().size());
InputStream stream = this.getClass().getResourceAsStream("PodTest.rkt");
Assert.assertNotNull("Could not open PodTest.rkt", stream);
doc = OpenRocketDocumentFactory.createEmptyRocket();
DocumentLoadingContext context = new DocumentLoadingContext();
context.setOpenRocketDocument(doc);
context.setMotorFinder(new DatabaseMotorFinder());
loader.loadFromStream(context, new BufferedInputStream(stream));
Assert.assertNotNull(doc);
rocket = doc.getRocket();
Assert.assertNotNull(rocket);
Assert.assertEquals(1, rocket.getStageCount());
AxialStage stage1 = (AxialStage) rocket.getChild(0);
Assert.assertEquals(3, stage1.getChildCount());
RocketComponent noseCone1 = stage1.getChild(0);
RocketComponent bodyTube1 = stage1.getChild(1);
RocketComponent transition1 = stage1.getChild(2);
Assert.assertEquals(NoseCone.class, noseCone1.getClass());
Assert.assertEquals(BodyTube.class, bodyTube1.getClass());
Assert.assertEquals(Transition.class, transition1.getClass());
Assert.assertEquals("Nose cone 1", noseCone1.getName());
Assert.assertEquals("Body tube 1", bodyTube1.getName());
Assert.assertEquals("Transition 1", transition1.getName());
Assert.assertEquals(1, noseCone1.getChildCount());
RocketComponent component = noseCone1.getChild(0);
Assert.assertEquals(MassComponent.class, component.getClass());
Assert.assertEquals("Mass object 1", component.getName());
Assert.assertEquals(2, bodyTube1.getChildCount());
RocketComponent pod2 = bodyTube1.getChild(0);
Assert.assertEquals(PodSet.class, pod2.getClass());
Assert.assertEquals("Pod 2", pod2.getName());
component = bodyTube1.getChild(1);
Assert.assertEquals(Bulkhead.class, component.getClass());
Assert.assertEquals("Bulkhead 1", component.getName());
Assert.assertEquals(3, pod2.getChildCount());
RocketComponent noseCone2 = pod2.getChild(0);
Assert.assertEquals(NoseCone.class, noseCone2.getClass());
Assert.assertEquals("Nose cone 2", noseCone2.getName());
RocketComponent bodyTube2 = pod2.getChild(1);
Assert.assertEquals(BodyTube.class, bodyTube2.getClass());
Assert.assertEquals("Body tube 2", bodyTube2.getName());
component = pod2.getChild(2);
Assert.assertEquals(Transition.class, component.getClass());
Assert.assertEquals("Transition 2", component.getName());
Assert.assertEquals(1, noseCone2.getChildCount());
component = noseCone2.getChild(0);
Assert.assertEquals(MassComponent.class, component.getClass());
Assert.assertEquals("Mass object 2", component.getName());
Assert.assertEquals(3, bodyTube2.getChildCount());
component = bodyTube2.getChild(0);
Assert.assertEquals(TrapezoidFinSet.class, component.getClass());
Assert.assertEquals("Fin set 2", component.getName());
RocketComponent pod3 = bodyTube2.getChild(1);
Assert.assertEquals(PodSet.class, pod3.getClass());
Assert.assertEquals("Pod 3", pod3.getName());
component = bodyTube2.getChild(2);
Assert.assertEquals(LaunchLug.class, component.getClass());
Assert.assertEquals("Launch lug 1", component.getName());
Assert.assertEquals(1, pod3.getChildCount());
component = pod3.getChild(0);
Assert.assertEquals(BodyTube.class, component.getClass());
Assert.assertEquals("Body tube 3", component.getName());
Assert.assertEquals(0.04, pod3.getAxialOffset(), MathUtil.EPSILON);
Assert.assertEquals(Math.PI / 2, pod3.getAngleOffset(), 0.0001);
Assert.assertEquals(0.05, pod3.getRadiusOffset(), MathUtil.EPSILON);
Assert.assertEquals(1, transition1.getChildCount());
component = transition1.getChild(0);
Assert.assertEquals(MassComponent.class, component.getClass());
Assert.assertEquals("Mass object 3", component.getName());
}
public static OpenRocketDocument loadRockSimRocket(RockSimLoader theLoader, String fileName) throws IOException, RocketLoadException {
try (InputStream stream = RockSimLoaderTest.class.getResourceAsStream(fileName)) {
Assert.assertNotNull("Could not open " + fileName, stream);

View File

@ -6,8 +6,6 @@ import net.sf.openrocket.rocketcomponent.FlightConfigurationId;
import net.sf.openrocket.rocketcomponent.Rocket;
import net.sf.openrocket.simulation.exception.MotorIgnitionException;
import net.sf.openrocket.simulation.exception.SimulationException;
import net.sf.openrocket.simulation.listeners.AbstractSimulationListener;
import net.sf.openrocket.simulation.listeners.SimulationListener;
import net.sf.openrocket.util.BaseTestCase.BaseTestCase;
import net.sf.openrocket.util.TestRockets;
import org.junit.Assert;
@ -35,11 +33,9 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getOptions().setISAAtmosphere(true);
simDisabled.getOptions().setTimeStep(0.05);
SimulationListener simulationListener = new AbstractSimulationListener();
// Since there are no stages, the simulation should throw an exception.
try {
simDisabled.simulate(simulationListener);
simDisabled.simulate();
} catch (SimulationException e) {
if (!(e instanceof MotorIgnitionException)) {
Assert.fail("Simulation should have thrown a MotorIgnitionException");
@ -56,7 +52,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getActiveConfiguration().setAllStages(); // Re-enable all stages.
compareSims(simOriginal, simDisabled, simulationListener, delta);
compareSims(simOriginal, simDisabled, delta);
}
/**
@ -83,9 +79,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getOptions().setISAAtmosphere(true);
simDisabled.getOptions().setTimeStep(0.05);
SimulationListener simulationListener = new AbstractSimulationListener();
compareSims(simRemoved, simDisabled, simulationListener, delta);
compareSims(simRemoved, simDisabled, delta);
//// Test re-enableing the stage.
Rocket rocketOriginal = TestRockets.makeBeta();
@ -96,7 +90,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getActiveConfiguration().setAllStages();
compareSims(simOriginal, simDisabled, simulationListener, delta);
compareSims(simOriginal, simDisabled, delta);
}
/**
@ -173,9 +167,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getOptions().setISAAtmosphere(true);
simDisabled.getOptions().setTimeStep(0.05);
SimulationListener simulationListener = new AbstractSimulationListener();
compareSims(simRemoved, simDisabled, simulationListener, delta);
compareSims(simRemoved, simDisabled, delta);
//// Test re-enableing the stage.
Rocket rocketOriginal = TestRockets.makeFalcon9Heavy();
@ -186,7 +178,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getActiveConfiguration().setAllStages();
compareSims(simOriginal, simDisabled, simulationListener, delta);
compareSims(simOriginal, simDisabled, delta);
}
/**
@ -214,11 +206,9 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getOptions().setISAAtmosphere(true);
simDisabled.getOptions().setTimeStep(0.05);
SimulationListener simulationListener = new AbstractSimulationListener();
// There should be no motors left at this point, so a no motors exception should be thrown
try {
simRemoved.simulate(simulationListener);
simRemoved.simulate();
} catch (SimulationException e) {
if (!(e instanceof MotorIgnitionException)) {
Assert.fail("Simulation failed: " + e);
@ -226,7 +216,7 @@ public class DisableStageTest extends BaseTestCase {
}
try {
simDisabled.simulate(simulationListener);
simDisabled.simulate();
} catch (SimulationException e) {
if (!(e instanceof MotorIgnitionException)) {
Assert.fail("Simulation failed: " + e);
@ -242,7 +232,7 @@ public class DisableStageTest extends BaseTestCase {
simDisabled.getActiveConfiguration().setAllStages();
compareSims(simOriginal, simDisabled, simulationListener, delta);
compareSims(simOriginal, simDisabled, delta);
}
/**
@ -259,13 +249,11 @@ public class DisableStageTest extends BaseTestCase {
* - groundHitVelocity
* @param simExpected the expected simulation results
* @param simActual the actual simulation results
* @param simulationListener the simulation listener to use for the comparison
* @param delta the error margin for the comparison (e.g. 0.05 = 5 % error margin)
*/
private void compareSims(Simulation simExpected, Simulation simActual,
SimulationListener simulationListener, double delta) {
private void compareSims(Simulation simExpected, Simulation simActual, double delta) {
try {
simExpected.simulate(simulationListener);
simExpected.simulate();
double maxAltitudeOriginal = simExpected.getSimulatedData().getMaxAltitude();
double maxVelocityOriginal = simExpected.getSimulatedData().getMaxVelocity();
double maxMachNumberOriginal = simExpected.getSimulatedData().getMaxMachNumber();
@ -274,7 +262,7 @@ public class DisableStageTest extends BaseTestCase {
double launchRodVelocityOriginal = simExpected.getSimulatedData().getLaunchRodVelocity();
double deploymentVelocityOriginal = simExpected.getSimulatedData().getDeploymentVelocity();
simActual.simulate(simulationListener);
simActual.simulate();
double maxAltitudeDisabled = simActual.getSimulatedData().getMaxAltitude();
double maxVelocityDisabled = simActual.getSimulatedData().getMaxVelocity();
double maxMachNumberDisabled = simActual.getSimulatedData().getMaxMachNumber();

View File

@ -0,0 +1,107 @@
package net.sf.openrocket.simulation;
import net.sf.openrocket.document.Simulation;
import net.sf.openrocket.rocketcomponent.FlightConfigurationId;
import net.sf.openrocket.rocketcomponent.Rocket;
import net.sf.openrocket.simulation.exception.SimulationException;
import net.sf.openrocket.util.BaseTestCase.BaseTestCase;
import net.sf.openrocket.util.TestRockets;
import org.junit.Test;
import java.util.List;
import java.util.stream.Collectors;
import static org.junit.Assert.assertEquals;
import static org.junit.Assert.assertSame;
/**
* Tests to verify that simulations contain all the expected flight events.
*/
public class FlightEventsTest extends BaseTestCase {
/**
* Tests for a single stage design.
*/
@Test
public void testSingleStage() throws SimulationException {
Rocket rocket = TestRockets.makeEstesAlphaIII();
Simulation sim = new Simulation(rocket);
sim.getOptions().setISAAtmosphere(true);
sim.getOptions().setTimeStep(0.05);
sim.setFlightConfigurationId(TestRockets.TEST_FCID_0);
sim.simulate();
// Test branch count
int branchCount = sim.getSimulatedData().getBranchCount();
assertEquals(" Single stage simulation invalid branch count", 1, branchCount);
FlightEvent.Type[] expectedEventTypes = {FlightEvent.Type.LAUNCH, FlightEvent.Type.IGNITION, FlightEvent.Type.LIFTOFF,
FlightEvent.Type.LAUNCHROD, FlightEvent.Type.BURNOUT, FlightEvent.Type.EJECTION_CHARGE, FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT,
FlightEvent.Type.APOGEE, FlightEvent.Type.GROUND_HIT, FlightEvent.Type.SIMULATION_END};
// Test event count
FlightDataBranch branch = sim.getSimulatedData().getBranch(0);
List<FlightEvent> eventList = branch.getEvents();
List<FlightEvent.Type> eventTypes = eventList.stream().map(FlightEvent::getType).collect(Collectors.toList());
assertEquals(" Single stage simulation invalid number of events", expectedEventTypes.length, eventTypes.size());
// Test that all expected events are present, and in the right order
for (int i = 0; i < expectedEventTypes.length; i++) {
assertSame(" Flight type " + expectedEventTypes[i] + " not found in single stage simulation",
eventTypes.get(i), expectedEventTypes[i]);
}
}
/**
* Tests for a multi-stage design.
*/
@Test
public void testMultiStage() throws SimulationException {
Rocket rocket = TestRockets.makeFalcon9Heavy();
Simulation sim = new Simulation(rocket);
sim.getOptions().setISAAtmosphere(true);
sim.getOptions().setTimeStep(0.05);
rocket.getSelectedConfiguration().setAllStages();
FlightConfigurationId fcid = rocket.getSelectedConfiguration().getFlightConfigurationID();
sim.setFlightConfigurationId(fcid);
sim.simulate();
// Test branch count
int branchCount = sim.getSimulatedData().getBranchCount();
assertEquals(" Multi-stage simulation invalid branch count", 3, branchCount);
for (int b = 0; b < 3; b++) {
FlightEvent.Type[] expectedEventTypes;
switch (b) {
case 0:
expectedEventTypes = new FlightEvent.Type[]{FlightEvent.Type.LAUNCH, FlightEvent.Type.IGNITION, FlightEvent.Type.IGNITION,
FlightEvent.Type.LIFTOFF, FlightEvent.Type.LAUNCHROD, FlightEvent.Type.APOGEE,
FlightEvent.Type.BURNOUT, FlightEvent.Type.EJECTION_CHARGE, FlightEvent.Type.STAGE_SEPARATION,
FlightEvent.Type.BURNOUT, FlightEvent.Type.EJECTION_CHARGE, FlightEvent.Type.STAGE_SEPARATION,
FlightEvent.Type.TUMBLE, FlightEvent.Type.GROUND_HIT, FlightEvent.Type.SIMULATION_END};
break;
case 1:
case 2:
expectedEventTypes = new FlightEvent.Type[]{FlightEvent.Type.TUMBLE, FlightEvent.Type.GROUND_HIT,
FlightEvent.Type.SIMULATION_END};
break;
default:
throw new IllegalStateException("Invalid branch number " + b);
}
// Test event count
FlightDataBranch branch = sim.getSimulatedData().getBranch(b);
List<FlightEvent> eventList = branch.getEvents();
List<FlightEvent.Type> eventTypes = eventList.stream().map(FlightEvent::getType).collect(Collectors.toList());
assertEquals(" Multi-stage simulation, branch " + b + " invalid number of events", expectedEventTypes.length, eventTypes.size());
// Test that all expected events are present, and in the right order
for (int i = 0; i < expectedEventTypes.length; i++) {
assertSame(" Flight type " + expectedEventTypes[i] + ", branch " + b + " not found in multi-stage simulation",
eventTypes.get(i), expectedEventTypes[i]);
}
}
}
}

View File

@ -13,6 +13,7 @@ import javax.swing.SpinnerNumberModel;
import javax.swing.event.ChangeEvent;
import javax.swing.event.ChangeListener;
import net.sf.openrocket.util.MathUtil;
import org.slf4j.Logger;
import org.slf4j.LoggerFactory;
@ -210,9 +211,16 @@ public class IntegerModel implements StateChangeListener {
* Sets the value of the variable.
*/
public void setValue(int v) {
int clampedValue = MathUtil.clamp(v, minValue, maxValue);
if (clampedValue != v) {
log.debug("Clamped value " + v + " to " + clampedValue + " for " + this);
v = clampedValue;
}
log.debug("Setting value " + v + " for " + this);
try {
setMethod.invoke(source, v);
fireStateChanged();
} catch (IllegalArgumentException e) {
throw new BugException(e);
} catch (IllegalAccessException e) {

View File

@ -86,7 +86,7 @@ public class ComponentAssemblyConfig extends RocketComponentConfig {
// set angle
JLabel angleLabel = new JLabel(trans.get("StageConfig.parallel.angle"));
motherPanel.add( angleLabel, "align left");
DoubleModel angleModel = new DoubleModel( boosters, "AngleOffset", 1.0, UnitGroup.UNITS_ANGLE, 0.0, Math.PI*2);
DoubleModel angleModel = new DoubleModel( boosters, "AngleOffset", 1.0, UnitGroup.UNITS_ANGLE, -Math.PI, Math.PI);
JSpinner angleSpinner = new JSpinner(angleModel.getSpinnerModel());
angleSpinner.setEditor(new SpinnerEditor(angleSpinner));

View File

@ -199,6 +199,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
@Override
public Object getValueAt(int row) {
Object c = stabData.get(row).name;
return c.toString();
}
@ -237,7 +238,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
@Override
public Object getValueAt(int row) {
return NOUNIT.toString(stabData.get(row).cpx);
return unit.toString(stabData.get(row).cpx);
}
},
new Column("<html>C<sub>N<sub>" + ALPHA + "</sub></sub>") {
@ -541,11 +542,6 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
rollData.clear();
for(final RocketComponent comp: configuration.getAllComponents()) {
// // this is actually redundant, because the analysis will not contain inactive stages.
// if (!configuration.isComponentActive(comp)) {
// continue;
// }
CMAnalysisEntry cmEntry = cmMap.get(comp.hashCode());
if (null == cmEntry) {
log.warn("Could not find massData entry for component: " + comp.getName());
@ -556,7 +552,11 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
continue;
}
LongitudinalStabilityRow row = new LongitudinalStabilityRow(cmEntry.name, cmEntry.source);
String name = cmEntry.name;
if (cmEntry.source instanceof Rocket) {
name = trans.get("componentanalysisdlg.TOTAL");
}
LongitudinalStabilityRow row = new LongitudinalStabilityRow(name, cmEntry.source);
stabData.add(row);
row.source = cmEntry.source;

View File

@ -504,8 +504,7 @@ public class SimulationPanel extends JPanel {
private void openDialog(final Simulation sim) {
boolean plotMode = false;
if (sim.hasSimulationData() && (sim.getStatus() == Status.UPTODATE || sim.getStatus() == Status.LOADED
|| sim.getStatus() == Status.EXTERNAL)) {
if (sim.hasSimulationData() && Simulation.isStatusUpToDate(sim.getStatus())) {
plotMode = true;
}
openDialog(plotMode, sim);

View File

@ -60,7 +60,7 @@ import org.jfree.ui.RectangleInsets;
import org.jfree.ui.TextAnchor;
/*
* It should be possible to simplify this code quite a bit by using a single Renderer instance for
* TODO: It should be possible to simplify this code quite a bit by using a single Renderer instance for
* both datasets and the legend. But for now, the renderers are queried for the line color information
* and this is held in the Legend.
*/

View File

@ -857,8 +857,8 @@ public class RocketPanel extends JPanel implements TreeSelectionListener, Change
// Re-run the present simulation(s)
List<Simulation> sims = new LinkedList<>();
for (Simulation sim : document.getSimulations()) {
if (sim.getStatus() == Simulation.Status.UPTODATE || sim.getStatus() == Simulation.Status.LOADED
|| !document.getRocket().getFlightConfiguration(sim.getFlightConfigurationId()).hasMotors())
if (Simulation.isStatusUpToDate(sim.getStatus()) ||
!document.getRocket().getFlightConfiguration(sim.getFlightConfigurationId()).hasMotors())
continue;
// Find a Simulation based on the current flight configuration

View File

@ -292,8 +292,7 @@ public class SimulationEditDialog extends JDialog {
@Override
public void actionPerformed(ActionEvent e) {
// If the simulation is out of date, run the simulation.
if (simulationList[0].getStatus() != Simulation.Status.UPTODATE &&
simulationList[0].getStatus() != Simulation.Status.LOADED) {
if (!Simulation.isStatusUpToDate(simulationList[0].getStatus())) {
new SimulationRunDialog(SimulationEditDialog.this.parentWindow, document, simulationList[0]).setVisible(true);
}