Merge with commit f8cfebe from kruland2607/openrocket

This commit is contained in:
Daniel_M_Williams 2016-01-01 16:04:33 -05:00
parent 206214e47a
commit 513e74fd15
8 changed files with 261 additions and 213 deletions

View File

@ -192,27 +192,27 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
// With the implementation of ParallelStages and Pods, this is no longer true. -Daniel Williams
//
// // Check for discontinuities
// if (component instanceof SymmetricComponent) {
// SymmetricComponent sym = (SymmetricComponent) component;
// // TODO:LOW: Ignores other cluster components (not clusterable)
// double x = component.toAbsolute(Coordinate.NUL)[0].x;
//
// // Check for lengthwise discontinuity
// if (x > componentX + 0.0001) {
// if (!MathUtil.equals(radius, 0)) {
// warnings.add(Warning.DISCONTINUITY);
// radius = 0;
// }
// }
// componentX = component.toAbsolute(new Coordinate(component.getLength()))[0].x;
//
// // Check for radius discontinuity
// if (!MathUtil.equals(sym.getForeRadius(), radius)) {
// warnings.add(Warning.DISCONTINUITY);
// // TODO: MEDIUM: Apply correction to values to cp and to map
// }
// radius = sym.getAftRadius();
// }
if (component instanceof SymmetricComponent) {
SymmetricComponent sym = (SymmetricComponent) component;
// TODO:LOW: Ignores other cluster components (not clusterable)
double x = component.toAbsolute(Coordinate.NUL)[0].x;
// Check for lengthwise discontinuity
if (x > componentX + 0.0001) {
if (!MathUtil.equals(radius, 0)) {
warnings.add(Warning.DISCONTINUITY);
radius = 0;
}
}
componentX = component.toAbsolute(new Coordinate(component.getLength()))[0].x;
// Check for radius discontinuity
if (!MathUtil.equals(sym.getForeRadius(), radius)) {
warnings.add(Warning.DISCONTINUITY);
// TODO: MEDIUM: Apply correction to values to cp and to map
}
radius = sym.getAftRadius();
}
// Call calculation method
forces.zero();

View File

@ -28,6 +28,7 @@ public class MassCalculator implements Monitorable {
public Coordinate getCG(Motor motor) {
return Coordinate.NUL;
}
},
LAUNCH_MASS {
@Override
@ -43,6 +44,25 @@ public class MassCalculator implements Monitorable {
};
public abstract Coordinate getCG(Motor motor);
/**
* Compute the cg contribution of the motor relative to the rocket's coordinates
*
* @param motorConfig
* @return
*/
public Coordinate getCG(MotorConfiguration motorConfig) {
Coordinate cg = getCG(motorConfig.getMotor());
cg = cg.add(motorConfig.getPosition());
RocketComponent motorMount = (RocketComponent) motorConfig.getMount();
Coordinate totalCG = new Coordinate();
for (Coordinate cord : motorMount.toAbsolute(cg) ) {
totalCG = totalCG.average(cord);
}
return totalCG;
}
}
private static final Logger log = LoggerFactory.getLogger(MassCalculator.class);
@ -151,7 +171,13 @@ public class MassCalculator implements Monitorable {
localCM = localCM.setWeight( localCM.weight * instanceCount);
// a *bit* hacky :P
Coordinate curMotorCM = localCM.setX( localCM.x + locations[0].x + motorXPosition );
// alternate version:
// double Ir = inst.getRotationalInertia();
// double It = inst.getLongitudinalInertia();
// +
// + Coordinate curMotorCM = type.getCG(inst);
double motorMass = curMotorCM.weight;
double Ir_single = mtrConfig.getUnitRotationalInertia()*motorMass;
double It_single = mtrConfig.getUnitLongitudinalInertia()*motorMass;

View File

@ -23,7 +23,6 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
protected boolean ignitionOveride = false;
protected double ignitionDelay = 0.0;
protected IgnitionEvent ignitionEvent = IgnitionEvent.NEVER;
protected double ignitionTime = 0.0;
protected int modID = 0;
@ -43,13 +42,11 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
public MotorState getSimulationState() {
MotorState state = motor.getNewInstance();
if( ignitionOveride ) {
state.setIgnitionTime( this.ignitionTime );
state.setIgnitionEvent( this.ignitionEvent );
state.setIgnitionDelay( this.ignitionDelay );
state.setEjectionDelay( this.ejectionDelay );
} else {
MotorConfiguration defInstance = mount.getDefaultMotorInstance();
state.setIgnitionTime( defInstance.ignitionTime );
state.setIgnitionEvent( defInstance.ignitionEvent );
state.setIgnitionDelay( defInstance.ignitionDelay );
state.setEjectionDelay( defInstance.ejectionDelay );
@ -110,20 +107,10 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
return mount.getLength() - motor.getLength() + mount.getMotorOverhang();
}
public double getIgnitionTime() {
return this.ignitionTime;
}
public void useDefaultIgnition() {
this.ignitionOveride = false;
}
public void setIgnitionTime(double _time) {
this.ignitionTime = _time;
this.ignitionOveride = true;
modID++;
}
public double getIgnitionDelay() {
return this.ignitionDelay;
}
@ -212,7 +199,6 @@ public class MotorConfiguration implements FlightConfigurableParameter<MotorConf
clone.ignitionOveride = this.ignitionOveride;
clone.ignitionDelay = this.ignitionDelay;
clone.ignitionEvent = this.ignitionEvent;
clone.ignitionTime = this.ignitionTime;
return clone;
}

View File

@ -164,6 +164,7 @@ public class FlightEvent implements Comparable<FlightEvent> {
@Override
public String toString() {
return "FlightEvent[type=" + type.name() + ",time=" + time + ",source=" + source + "]";
return "FlightEvent[type=" + type.name() + ",time=" + time + ",source=" + source + ",data=" + String.valueOf(data) + "]";
}
}

View File

@ -432,23 +432,6 @@ public class TestRockets {
return rocket;
}
// This function is used for unit, integration tests, DO NOT CHANGE (without updating tests).
public static final MotorConfiguration getTestD12Motor() {
// Estes D12:
// http://nar.org/SandT/pdf/Estes/D12.pdf
ThrustCurveMotor motor = new ThrustCurveMotor(
Manufacturer.getManufacturer("Estes"),
"D12-X", "Test Motor", Motor.Type.SINGLE, new double[] {0,3,5,7},
0.024, 0.07, new double[] { 0, 1, 2 }, new double[] { 0, 10.2, 0 },
new Coordinate[] { new Coordinate(0.0035,0,0,44.0),
new Coordinate(0.0035,0,0,30.0),
new Coordinate(0.0035,0,0,21.0)},
"digest_D12");
MotorConfiguration inst = new MotorConfiguration(motor);
inst.setEjectionDelay(5);
return inst;
}
public static Rocket makeSmallFlyable() {
double noseconeLength = 0.10, noseconeRadius = 0.01;
double bodytubeLength = 0.20, bodytubeRadius = 0.01, bodytubeThickness = 0.001;

View File

@ -11,11 +11,8 @@ import com.google.inject.Injector;
import com.google.inject.Module;
import net.sf.openrocket.ServicesForTesting;
import net.sf.openrocket.motor.MotorConfiguration;
import net.sf.openrocket.plugin.PluginModule;
import net.sf.openrocket.rocketcomponent.FlightConfiguration;
import net.sf.openrocket.rocketcomponent.FlightConfigurationId;
import net.sf.openrocket.rocketcomponent.InnerTube;
import net.sf.openrocket.rocketcomponent.Rocket;
import net.sf.openrocket.startup.Application;
import net.sf.openrocket.util.Coordinate;
@ -64,16 +61,10 @@ public class BarrowmanCalculatorTest {
public void testCPSimpleWithMotor() {
Rocket rkt = TestRockets.makeEstesAlphaIII();
FlightConfiguration config = rkt.getSelectedConfiguration();
FlightConfigurationId fcid = config.getFlightConfigurationID();
AerodynamicCalculator calc = new BarrowmanCalculator();
FlightConditions conditions = new FlightConditions(config);
WarningSet warnings = new WarningSet();
MotorConfiguration inst = TestRockets.getTestD12Motor();
InnerTube motorTube = (InnerTube)rkt.getChild(0).getChild(1).getChild(1);
motorTube.setMotorInstance(fcid, inst);
motorTube.setMotorMount(true);
motorTube.setMotorOverhang(0.005);
// calculated from OpenRocket 15.03
double expCPx = 0.225; // cm

View File

@ -50,7 +50,7 @@ public class ParallelStageTest extends BaseTestCase {
FinSet coreFins = new TrapezoidFinSet(4, 4, 2, 2, 4);
coreFins.setName("Core Fins");
coreLowerBody.addChild(coreFins);
rocket.enableEvents();
return rocket;
}

View File

@ -55,9 +55,10 @@ import net.sf.openrocket.gui.util.GUIUtil;
import net.sf.openrocket.l10n.Translator;
import net.sf.openrocket.masscalc.MassCalculator;
import net.sf.openrocket.masscalc.MassCalculator.MassCalcType;
import net.sf.openrocket.motor.MotorConfiguration;
import net.sf.openrocket.rocketcomponent.AxialStage;
import net.sf.openrocket.rocketcomponent.FinSet;
import net.sf.openrocket.rocketcomponent.FlightConfiguration;
import net.sf.openrocket.rocketcomponent.FlightConfigurationId;
import net.sf.openrocket.rocketcomponent.Rocket;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.startup.Application;
@ -71,8 +72,8 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
private static final long serialVersionUID = 9131240570600307935L;
private static ComponentAnalysisDialog singletonDialog = null;
private static final Translator trans = Application.getTranslator();
private final FlightConditions conditions;
private final FlightConfiguration configuration;
private final DoubleModel theta, aoa, mach, roll;
@ -80,37 +81,36 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
private boolean fakeChange = false;
private AerodynamicCalculator aerodynamicCalculator;
private final MassCalculator massCalculator = new MassCalculator();
private final ColumnTableModel cpTableModel;
private final ColumnTableModel dragTableModel;
private final ColumnTableModel rollTableModel;
private final JList warningList;
private final List<AerodynamicForces> cpData = new ArrayList<AerodynamicForces>();
private final List<Coordinate> cgData = new ArrayList<Coordinate>();
private final JList<Object> warningList;
private final List<Object[]> cgData = new ArrayList<Object[]>();
private final List<AerodynamicForces> dragData = new ArrayList<AerodynamicForces>();
private double totalCD = 0;
private final List<AerodynamicForces> rollData = new ArrayList<AerodynamicForces>();
public ComponentAnalysisDialog(final RocketPanel rocketPanel) {
////Component analysis
super(SwingUtilities.getWindowAncestor(rocketPanel),
trans.get("componentanalysisdlg.componentanalysis"));
JTable table;
JPanel panel = new JPanel(new MigLayout("fill", "[][35lp::][fill][fill]"));
JPanel panel = new JPanel(new MigLayout("fill"));
add(panel);
this.configuration = rocketPanel.getConfiguration();
this.aerodynamicCalculator = rocketPanel.getAerodynamicCalculator().newInstance();
conditions = new FlightConditions(configuration);
rocketPanel.setCPAOA(0);
aoa = new DoubleModel(rocketPanel, "CPAOA", UnitGroup.UNITS_ANGLE, 0, Math.PI);
rocketPanel.setCPMach(Application.getPreferences().getDefaultMach());
@ -119,7 +119,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
theta = new DoubleModel(rocketPanel, "CPTheta", UnitGroup.UNITS_ANGLE, 0, 2 * Math.PI);
rocketPanel.setCPRoll(0);
roll = new DoubleModel(rocketPanel, "CPRoll", UnitGroup.UNITS_ROLL);
//// Wind direction:
panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.winddir")), "width 120lp!");
panel.add(new UnitSelector(theta, true), "width 50lp!");
@ -142,59 +142,59 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
}
});
panel.add(worstToggle, "");
warningList = new JList();
warningList = new JList<>();
JScrollPane scrollPane = new JScrollPane(warningList);
////Warnings:
scrollPane.setBorder(BorderFactory.createTitledBorder(trans.get("componentanalysisdlg.TitledBorder.warnings")));
panel.add(scrollPane, "gap paragraph, spany 4, width 300lp!, growy 1, height :100lp:, wrap");
////Angle of attack:
panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.angleofattack")), "width 120lp!");
panel.add(new UnitSelector(aoa, true), "width 50lp!");
panel.add(new BasicSlider(aoa.getSliderModel(0, Math.PI)), "growx, wrap");
//// Mach number:
panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.machnumber")), "width 120lp!");
panel.add(new UnitSelector(mach, true), "width 50lp!");
panel.add(new BasicSlider(mach.getSliderModel(0, 3)), "growx, wrap");
//// Roll rate:
panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.rollrate")), "width 120lp!");
panel.add(new UnitSelector(roll, true), "width 50lp!");
panel.add(new BasicSlider(roll.getSliderModel(-20 * 2 * Math.PI, 20 * 2 * Math.PI)),
"growx, wrap paragraph");
"growx, wrap");
// Stage and motor selection:
//// Active stages:
panel.add(new JLabel(trans.get("componentanalysisdlg.lbl.activestages")), "spanx, split, gapafter rel");
panel.add(new StageSelector(configuration), "gapafter paragraph");
//// Motor configuration:
JLabel label = new JLabel(trans.get("componentanalysisdlg.lbl.motorconf"));
label.setHorizontalAlignment(JLabel.RIGHT);
panel.add(label, "growx, right");
JComboBox<FlightConfiguration> combo = new JComboBox<FlightConfiguration>( configuration.getRocket().toConfigArray());
panel.add(combo, "wrap");
// Tabbed pane
JTabbedPane tabbedPane = new JTabbedPane();
panel.add(tabbedPane, "spanx, growx, growy");
// Create the CP data table
cpTableModel = new ColumnTableModel(
//// Component
new Column(trans.get("componentanalysisdlg.TabStability.Col.Component")) {
@Override
public Object getValueAt(int row) {
RocketComponent c = cpData.get(row).getComponent();
Object c = cgData.get(row)[0];
if (c instanceof Rocket) {
return trans.get("componentanalysisdlg.TOTAL");
}
@ -211,7 +211,11 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
@Override
public Object getValueAt(int row) {
return unit.toString(cgData.get(row).x);
Coordinate cg = (Coordinate) cgData.get(row)[1];
if ( cg == null ) {
return null;
}
return unit.toString(cg.x);
}
},
new Column(trans.get("componentanalysisdlg.TabStability.Col.Mass") + " / " + UnitGroup.UNITS_MASS.getDefaultUnit().getUnit()) {
@ -219,7 +223,11 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
@Override
public Object getValueAt(int row) {
return unit.toString(cgData.get(row).weight);
Coordinate cg = (Coordinate) cgData.get(row)[1];
if ( cg == null ) {
return null;
}
return unit.toString(cg.weight);
}
},
new Column(trans.get("componentanalysisdlg.TabStability.Col.CP") + " / " + UnitGroup.UNITS_LENGTH.getDefaultUnit().getUnit()) {
@ -227,42 +235,56 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
@Override
public Object getValueAt(int row) {
return unit.toString(cpData.get(row).getCP().x);
AerodynamicForces forces = (AerodynamicForces) cgData.get(row)[2];
if ( forces == null ) {
return null;
}
return unit.toString(forces.getCP().x);
}
},
new Column("<html>C<sub>N<sub>" + ALPHA + "</sub></sub>") {
@Override
public Object getValueAt(int row) {
return NOUNIT.toString(cpData.get(row).getCP().weight);
AerodynamicForces forces = (AerodynamicForces) cgData.get(row)[2];
if ( forces == null ) {
return null;
}
return NOUNIT.toString(forces.getCP().weight);
}
}
) {
@Override
public int getRowCount() {
return cpData.size();
}
};
/**
*
*/
private static final long serialVersionUID = 1L;
@Override
public int getRowCount() {
return cgData.size();
}
};
table = new ColumnTable(cpTableModel);
table.setSelectionMode(ListSelectionModel.SINGLE_SELECTION);
table.setSelectionBackground(Color.LIGHT_GRAY);
table.setSelectionForeground(Color.BLACK);
cpTableModel.setColumnWidths(table.getColumnModel());
table.setDefaultRenderer(Object.class, new CustomCellRenderer());
// table.setShowHorizontalLines(false);
// table.setShowVerticalLines(true);
JScrollPane scrollpane = new JScrollPane(table);
scrollpane.setPreferredSize(new Dimension(600, 200));
//// Stability and Stability information
tabbedPane.addTab(trans.get("componentanalysisdlg.TabStability"),
null, scrollpane, trans.get("componentanalysisdlg.TabStability.ttip"));
// Create the drag data table
dragTableModel = new ColumnTableModel(
//// Component
@ -275,7 +297,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
}
return c.toString();
}
@Override
public int getDefaultWidth() {
return 200;
@ -310,33 +332,38 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
}
}
) {
@Override
public int getRowCount() {
return dragData.size();
}
};
/**
*
*/
private static final long serialVersionUID = 1L;
@Override
public int getRowCount() {
return dragData.size();
}
};
table = new JTable(dragTableModel);
table.setSelectionMode(ListSelectionModel.SINGLE_SELECTION);
table.setSelectionBackground(Color.LIGHT_GRAY);
table.setSelectionForeground(Color.BLACK);
dragTableModel.setColumnWidths(table.getColumnModel());
table.setDefaultRenderer(Object.class, new DragCellRenderer(new Color(0.5f, 1.0f, 0.5f)));
// table.setShowHorizontalLines(false);
// table.setShowVerticalLines(true);
scrollpane = new JScrollPane(table);
scrollpane.setPreferredSize(new Dimension(600, 200));
//// Drag characteristics and Drag characteristics tooltip
tabbedPane.addTab(trans.get("componentanalysisdlg.dragTabchar"), null, scrollpane,
trans.get("componentanalysisdlg.dragTabchar.ttip"));
// Create the roll data table
rollTableModel = new ColumnTableModel(
//// Component
@ -372,39 +399,44 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
}
}
) {
@Override
public int getRowCount() {
return rollData.size();
}
};
/**
*
*/
private static final long serialVersionUID = 1L;
@Override
public int getRowCount() {
return rollData.size();
}
};
table = new JTable(rollTableModel);
table.setSelectionMode(ListSelectionModel.SINGLE_SELECTION);
table.setSelectionBackground(Color.LIGHT_GRAY);
table.setSelectionForeground(Color.BLACK);
rollTableModel.setColumnWidths(table.getColumnModel());
table.setDefaultRenderer(Object.class, new CustomCellRenderer());
scrollpane = new JScrollPane(table);
scrollpane.setPreferredSize(new Dimension(600, 200));
//// Roll dynamics and Roll dynamics tooltip
tabbedPane.addTab(trans.get("componentanalysisdlg.rollTableModel"), null, scrollpane,
trans.get("componentanalysisdlg.rollTableModel.ttip"));
// Add the data updater to listen to changes in aoa and theta
mach.addChangeListener(this);
theta.addChangeListener(this);
aoa.addChangeListener(this);
roll.addChangeListener(this);
this.stateChanged(null);
// Remove listeners when closing window
this.addWindowListener(new WindowAdapter() {
@Override
@ -422,7 +454,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
singletonDialog = null;
}
});
//// Reference length:
panel.add(new StyledLabel(trans.get("componentanalysisdlg.lbl.reflenght"), -1),
"span, split, gapleft para, gapright rel");
@ -430,19 +462,19 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
UnitSelector sel = new UnitSelector(dm, true);
sel.resizeFont(-1);
panel.add(sel, "gapright para");
//// Reference area:
panel.add(new StyledLabel(trans.get("componentanalysisdlg.lbl.refarea"), -1), "gapright rel");
dm = new DoubleModel(conditions, "RefArea", UnitGroup.UNITS_AREA);
sel = new UnitSelector(dm, true);
sel.resizeFont(-1);
panel.add(sel, "wrap");
// Buttons
JButton button;
// TODO: LOW: printing
// button = new JButton("Print");
// button.addActionListener(new ActionListener() {
@ -457,7 +489,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
// }
// });
// panel.add(button,"tag ok");
//button = new JButton("Close");
//Close button
button = new JButton(trans.get("dlg.but.close"));
@ -467,18 +499,18 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
ComponentAnalysisDialog.this.dispose();
}
});
panel.add(button, "span, split, tag cancel");
panel.add(button, "span, tag cancel");
this.setLocationByPlatform(true);
setDefaultCloseOperation(JFrame.DISPOSE_ON_CLOSE);
pack();
GUIUtil.setDisposableDialogOptions(this, null);
}
/**
* Updates the data in the table and fires a table data change event.
*/
@ -491,7 +523,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
conditions.setMach(mach.getValue());
conditions.setRollRate(roll.getValue());
conditions.setReference(configuration);
if (worstToggle.isSelected()) {
aerodynamicCalculator.getWorstCP(configuration, conditions, null);
if (!MathUtil.equals(conditions.getTheta(), theta.getValue())) {
@ -501,27 +533,35 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
return;
}
}
Map<RocketComponent, AerodynamicForces> aeroData =
aerodynamicCalculator.getForceAnalysis(configuration, conditions, set);
Map<RocketComponent, Coordinate> massData =
massCalculator.getCGAnalysis(configuration, MassCalcType.LAUNCH_MASS);
cpData.clear();
cgData.clear();
dragData.clear();
rollData.clear();
for (RocketComponent c : configuration.getActiveComponents()) {
forces = aeroData.get(c);
Coordinate cg = massData.get(c);
if (forces == null)
if ( c instanceof AxialStage ) {
continue;
if (forces.getCP() != null) {
cpData.add(forces);
cgData.add(cg);
}
Object[] data = new Object[3];
cgData.add(data);
data[0] = c;
Coordinate cg = massData.get(c);
data[1] = cg;
forces = aeroData.get(c);
if (forces == null) {
continue;
}
if (forces.getCP() != null) {
data[2] = forces;
}
if (!Double.isNaN(forces.getCD())) {
dragData.add(forces);
}
@ -529,17 +569,30 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
rollData.add(forces);
}
}
for ( MotorConfiguration motorConfig : configuration.getActiveMotors()) {
Object [] data = new Object[3];
cgData.add(data);
data[0] = motorConfig.getMotor().getDesignation();
data[1] = MassCalcType.LAUNCH_MASS.getCG(motorConfig);
}
forces = aeroData.get(configuration.getRocket());
if (forces != null) {
cpData.add(forces);
cgData.add(massData.get(configuration.getRocket()));
Object[] data = new Object[3];
cgData.add(data);
data[0] = configuration.getRocket();
data[1] = massData.get(configuration.getRocket());
data[2] = forces;
dragData.add(forces);
rollData.add(forces);
totalCD = forces.getCD();
} else {
totalCD = 0;
}
// Set warnings
if (set.isEmpty()) {
warningList.setListData(new String[] {
@ -548,33 +601,37 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
} else {
warningList.setListData(new Vector<Warning>(set));
}
cpTableModel.fireTableDataChanged();
dragTableModel.fireTableDataChanged();
rollTableModel.fireTableDataChanged();
}
private class CustomCellRenderer extends JLabel implements TableCellRenderer {
/**
*
*/
private static final long serialVersionUID = 1L;
private final Font normalFont;
private final Font boldFont;
public CustomCellRenderer() {
super();
normalFont = getFont();
boldFont = normalFont.deriveFont(Font.BOLD);
}
@Override
public Component getTableCellRendererComponent(JTable table, Object value,
boolean isSelected, boolean hasFocus, int row, int column) {
this.setText(value.toString());
if ((row < 0) || (row >= cpData.size()))
this.setText(value == null ? null : value.toString());
if ((row < 0) || (row >= cgData.size()))
return this;
if (cpData.get(row).getComponent() instanceof Rocket) {
if (cgData.get(row)[0] instanceof Rocket) {
this.setFont(boldFont);
} else {
this.setFont(normalFont);
@ -582,52 +639,56 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
return this;
}
}
private class DragCellRenderer extends JLabel implements TableCellRenderer {
/**
*
*/
private static final long serialVersionUID = 1L;
private final Font normalFont;
private final Font boldFont;
public DragCellRenderer(Color baseColor) {
super();
normalFont = getFont();
boldFont = normalFont.deriveFont(Font.BOLD);
}
@Override
public Component getTableCellRendererComponent(JTable table, Object value,
boolean isSelected, boolean hasFocus, int row, int column) {
if (value instanceof Double) {
// A drag coefficient
double cd = (Double) value;
this.setText(String.format("%.2f (%.0f%%)", cd, 100 * cd / totalCD));
float r = (float) (cd / 1.5);
float hue = MathUtil.clamp(0.3333f * (1 - 2.0f * r), 0, 0.3333f);
float sat = MathUtil.clamp(0.8f * r + 0.1f * (1 - r), 0, 1);
float val = 1.0f;
this.setBackground(Color.getHSBColor(hue, sat, val));
this.setOpaque(true);
this.setHorizontalAlignment(SwingConstants.CENTER);
} else {
// Other
this.setText(value.toString());
this.setOpaque(false);
this.setHorizontalAlignment(SwingConstants.LEFT);
}
if ((row < 0) || (row >= dragData.size()))
return this;
if ((dragData.get(row).getComponent() instanceof Rocket) || (column == 4)) {
this.setFont(boldFont);
} else {
@ -636,20 +697,20 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
return this;
}
}
///////// Singleton implementation
public static void showDialog(RocketPanel rocketpanel) {
if (singletonDialog != null)
singletonDialog.dispose();
singletonDialog = new ComponentAnalysisDialog(rocketpanel);
singletonDialog.setVisible(true);
}
public static void hideDialog() {
if (singletonDialog != null)
singletonDialog.dispose();
}
}