Merge pull request #676 from teyrana/509-fix-component-analysis

[fixes #509] Fix Component Analysis Dialog

core/resources/l10n/messages.properties

@@ -700,9 +700,10 @@ componentanalysisdlg.lbl.machnumber = Mach number:
 componentanalysisdlg.lbl.rollrate = Roll rate:
 componentanalysisdlg.lbl.activestages = Active stages:
 componentanalysisdlg.lbl.motorconf = Motor configuration:
-componentanalysisdlg.TabStability.Col = Component
+componentanalysisdlg.TabStability.Col = Component Name
-componentanalysisdlg.TabStability.Col.CG = CG
+componentanalysisdlg.TabStability.Col.EachMass = Instance Mass
-componentanalysisdlg.TabStability.Col.Mass = Mass
+componentanalysisdlg.TabStability.Col.AllMass = Aggregate Mass
+componentanalysisdlg.TabStability.Col.CG = Aggregate CG Location
 componentanalysisdlg.TabStability.Col.CP = CP
 componentanalysisdlg.TabStability = Stability
 componentanalysisdlg.TabStability.ttip = Stability information

core/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java

@@ -2,14 +2,7 @@ package net.sf.openrocket.aerodynamics;
 
 import static net.sf.openrocket.util.MathUtil.pow2;
 
-import java.util.ArrayList;
+import java.util.*;
-import java.util.Arrays;
-import java.util.HashMap;
-import java.util.Iterator;
-import java.util.LinkedHashMap;
-import java.util.LinkedList;
-import java.util.Map;
-import java.util.Queue;
 
 import net.sf.openrocket.aerodynamics.barrowman.FinSetCalc;
 import net.sf.openrocket.aerodynamics.barrowman.RocketComponentCalc;
@@ -27,7 +20,7 @@ import net.sf.openrocket.util.Coordinate;
 import net.sf.openrocket.util.MathUtil;
 import net.sf.openrocket.util.PolyInterpolator;
 import net.sf.openrocket.util.Reflection;
-import net.sf.openrocket.util.Transformation;
+
 
 /**
  * An aerodynamic calculator that uses the extended Barrowman method to 
@@ -64,7 +57,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	public Coordinate getCP(FlightConfiguration configuration, FlightConditions conditions,
 			WarningSet warnings) {
 		checkCache(configuration);
-		AerodynamicForces forces = calculateNonAxialForces(configuration, conditions, null, warnings);
+		AerodynamicForces forces = calculateNonAxialForces(configuration, conditions, warnings);
 		return forces.getCP();
 	}
 	
@@ -72,60 +65,102 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	
 	@Override
 	public Map<RocketComponent, AerodynamicForces> getForceAnalysis(FlightConfiguration configuration,
-			FlightConditions conditions, WarningSet warnings) {
+																	FlightConditions conditions,
-		checkCache(configuration);
+																	WarningSet warnings) {
-		
+		if (calcMap == null){
-		AerodynamicForces f;
+			buildCalcMap(configuration);
-		Map<RocketComponent, AerodynamicForces> map =
-				new LinkedHashMap<RocketComponent, AerodynamicForces>();
-		
-		// Add all components to the map
-		for (RocketComponent component : configuration.getActiveComponents()) {
-			
-			// Skip non-aerodynamic components
-			if (!component.isAerodynamic())
-				continue;
-			
-			f = new AerodynamicForces();
-			f.setComponent(component);
-			
-			map.put(component, f);
 		}
-		
+
-		
+		InstanceMap instMap = configuration.getActiveInstances();
+		Map<RocketComponent, AerodynamicForces> eachMap = new LinkedHashMap<>();
+		Map<RocketComponent, AerodynamicForces> assemblyMap = new LinkedHashMap<>();
+
 		// Calculate non-axial force data
-		AerodynamicForces total = calculateNonAxialForces(configuration, conditions, map, warnings);
+		calculateForceAnalysis(conditions, configuration.getRocket(), instMap, eachMap, assemblyMap, warnings);
-		
+
-		
 		// Calculate friction data
-		total.setFrictionCD(calculateFrictionDrag(configuration, conditions, map, warnings));
+		AerodynamicForces rocketForces = assemblyMap.get(configuration.getRocket());
-		total.setPressureCD(calculatePressureDrag(configuration, conditions, map, warnings));
+		rocketForces.setFrictionCD(calculateFrictionDrag(configuration, conditions, eachMap, warnings));
-		total.setBaseCD(calculateBaseDrag(configuration, conditions, map, warnings));
+		rocketForces.setPressureCD(calculatePressureDrag(configuration, conditions, eachMap, warnings));
-		
+		rocketForces.setBaseCD(calculateBaseDrag(configuration, conditions, eachMap, warnings));
-		total.setComponent(configuration.getRocket());
+
-		map.put(total.getComponent(), total);
+		Map<RocketComponent, AerodynamicForces> finalMap = new LinkedHashMap<>();
-		
+		for(final RocketComponent comp : instMap.keySet()){
-		
+
-		for (RocketComponent c : map.keySet()) {
+			AerodynamicForces f;
-			f = map.get(c);
+			if(comp instanceof ComponentAssembly) {
-			if (Double.isNaN(f.getBaseCD()) && Double.isNaN(f.getPressureCD()) &&
+				f = assemblyMap.get(comp);
-					Double.isNaN(f.getFrictionCD()))
+			} else if(comp.isAerodynamic()){
+				f = eachMap.get(comp);
+			}else{
 				continue;
+			}
+
+			if (Double.isNaN(f.getCNa())){
+				f.setCNa(0.0);
+			}
+			if (f.getCP().isNaN()) {
+				f.setCP(Coordinate.ZERO);
+			}
+
 			if (Double.isNaN(f.getBaseCD()))
 				f.setBaseCD(0);
+
 			if (Double.isNaN(f.getPressureCD()))
 				f.setPressureCD(0);
+
 			if (Double.isNaN(f.getFrictionCD()))
 				f.setFrictionCD(0);
+
 			f.setCD(f.getBaseCD() + f.getPressureCD() + f.getFrictionCD());
 			f.setCaxial(calculateAxialDrag(conditions, f.getCD()));
+
+			finalMap.put(comp, f);
 		}
-		
+
-		return map;
+		return finalMap;
 	}
-	
+
-	
+	private AerodynamicForces calculateForceAnalysis(   FlightConditions conds,
-	
+														RocketComponent comp,
+														InstanceMap instances,
+														Map<RocketComponent, AerodynamicForces> eachForces,
+														Map<RocketComponent, AerodynamicForces> assemblyForces,
+														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()) {
+			RocketComponentCalc calcObj = calcMap.get(comp);
+			if (null == calcObj) {
+				throw new NullPointerException("Could not find a CalculationObject for aerodynamic Component!: " + comp.getComponentName());
+			} else {
+				List<InstanceContext> contextList = instances.get(comp);
+				// across every instance of this component:
+				AerodynamicForces compForces = calculateComponentNonAxialForces(conds, comp, calcObj, contextList, warnings);
+				eachForces.put(comp, compForces);
+				aggregateForces.merge(compForces);
+			}
+		}
+
+		for( RocketComponent child : comp.getChildren()) {
+			// forces particular to each component
+			AerodynamicForces childForces = calculateForceAnalysis(conds, child, instances, eachForces, assemblyForces, warnings);
+
+			if(null != childForces) {
+				aggregateForces.merge(childForces);
+			}
+		}
+
+		assemblyForces.put(comp, aggregateForces);
+
+		return eachForces.get(comp);
+	}
+
 	@Override
 	public AerodynamicForces getAerodynamicForces(FlightConfiguration configuration,
 			FlightConditions conditions, WarningSet warnings) {
@@ -135,7 +170,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 			warnings = ignoreWarningSet;
 		
 		// Calculate non-axial force data
-		AerodynamicForces total = calculateNonAxialForces(configuration, conditions, null, warnings);
+		AerodynamicForces total = calculateNonAxialForces(configuration, conditions, warnings);
 		
 		// Calculate friction data
 		total.setFrictionCD(calculateFrictionDrag(configuration, conditions, null, warnings));
@@ -150,77 +185,79 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 		calculateDampingMoments(configuration, conditions, total);
 		total.setCm(total.getCm() - total.getPitchDampingMoment());
 		total.setCyaw(total.getCyaw() - total.getYawDampingMoment());
-		
+
-		
 		return total;
 	}
-	
+
-	
+
+	private AerodynamicForces calculateComponentNonAxialForces( FlightConditions conditions,
+																RocketComponent comp,
+																RocketComponentCalc calcObj,
+																List<InstanceContext> contextList,
+																WarningSet warnings)
+	{
+		// across every instance of this component:
+		final AerodynamicForces componentForces = new AerodynamicForces().zero();
+
+		// iterate across component instances
+		for(InstanceContext context: contextList ) {
+			// specific to this _instance_ of this component:
+			AerodynamicForces instanceForces = new AerodynamicForces().zero();
+			calcObj.calculateNonaxialForces(conditions, context.transform, instanceForces, warnings);
+
+			Coordinate cp_inst = instanceForces.getCP();
+			Coordinate cp_abs = context.transform.transform(cp_inst);
+			cp_abs = cp_abs.setY(0.0).setZ(0.0);
+
+			instanceForces.setCP(cp_abs);
+			double CN_instanced = instanceForces.getCN();
+			instanceForces.setCm(CN_instanced * instanceForces.getCP().x / conditions.getRefLength());
+
+			componentForces.merge(instanceForces);
+		}
+		componentForces.setComponent(comp);
+
+		return componentForces;
+	}
 
 	/**
 	 * Perform the actual CP calculation.
 	 */
-	private AerodynamicForces calculateNonAxialForces(FlightConfiguration configuration, FlightConditions conditions,
+	private AerodynamicForces calculateNonAxialForces(FlightConfiguration configuration, FlightConditions conditions, WarningSet warnings) {
-			Map<RocketComponent, AerodynamicForces> calculators, WarningSet warnings) {
+
-		
 		checkCache(configuration);
-		
+
 		if (warnings == null)
 			warnings = ignoreWarningSet;
-		
+
 		if (conditions.getAOA() > 17.5 * Math.PI / 180)
 			warnings.add(new Warning.LargeAOA(conditions.getAOA()));
-		
+
 		if (calcMap == null)
 			buildCalcMap(configuration);
 		
-		
 		if( ! isContinuous(  configuration.getRocket() ) ){
 			warnings.add( Warning.DIAMETER_DISCONTINUITY);
 		}
 		
 		final InstanceMap imap = configuration.getActiveInstances();
-		
+
+		// across the _entire_ assembly -- like a rocket, or a stage
 		final AerodynamicForces assemblyForces= new AerodynamicForces().zero();
 
-//		System.err.println("======================================");
+		for(Map.Entry<RocketComponent, ArrayList<InstanceContext>> mapEntry: imap.entrySet() ) {
-//		System.err.println("==== Iterating through components ====");
+			final RocketComponent comp = mapEntry.getKey();
-		// iterate through all components
+			final List<InstanceContext> contextList = mapEntry.getValue();
-	    for(Map.Entry<RocketComponent, ArrayList<InstanceContext>> entry: imap.entrySet() ) {
+
-			final RocketComponent comp = entry.getKey();
 			RocketComponentCalc calcObj = calcMap.get(comp);
-
-			// System.err.println("comp=" + comp);
 			if (null != calcObj) {
-				// iterate across component instances
+				// calculated across all component instances
-				final ArrayList<InstanceContext> contextList = entry.getValue();
+				final AerodynamicForces componentForces = calculateComponentNonAxialForces(conditions, comp, calcObj, contextList, warnings);
 
-				for(InstanceContext context: contextList ) {
+				assemblyForces.merge(componentForces);
-					AerodynamicForces instanceForces = new AerodynamicForces().zero();
-//					System.err.println(String.format("@ [%s]:[%d/%d]", comp.getName(), context.instanceNumber + 1, comp.getInstanceCount()));
-//					System.err.println("_________ inst/ctxt: xrotation: " + context.transform.getXrotation());
-					
-					calcObj.calculateNonaxialForces(conditions, context.transform, instanceForces, warnings);
-					
-					Coordinate cp_inst = instanceForces.getCP();
-					Coordinate cp_abs = context.transform.transform(cp_inst);
-					cp_abs = cp_abs.setY(0.0).setZ(0.0);
-					
-//					if( 1e-6 < cp_inst.weight) {
-//						System.err.println("_________ cp:inst: (rel): " + cp_inst.toString());
-//						System.err.println("_________ cp:inst: (abs): " + cp_abs.toString());
-//					}
-					
-					instanceForces.setCP(cp_abs);
-					double CN_instanced = instanceForces.getCN();
-					instanceForces.setCm(CN_instanced * instanceForces.getCP().x / conditions.getRefLength());
-					assemblyForces.merge(instanceForces);
-					
-				}
 			}
 		}
 
-//		System.err.println("____ cp:asbly: " + assemblyForces.getCP().toString());
 		return assemblyForces;
 	}
 	
@@ -230,7 +267,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	}
 	
 	private boolean testIsContinuous( final RocketComponent treeRoot ){
-		Queue<RocketComponent> queue = new LinkedList<RocketComponent>();
+		Queue<RocketComponent> queue = new LinkedList<>();
 		queue.addAll(treeRoot.getChildren());
 		
 		boolean isContinuous = true;
@@ -279,7 +316,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	 * @param conditions		Flight conditions taken into account
 	 * @param map				?
 	 * @param set				Set to handle 
-	 * @return
+	 * @return friction drag for entire rocket
 	 */
 	private double calculateFrictionDrag(FlightConfiguration configuration, FlightConditions conditions,
 			Map<RocketComponent, AerodynamicForces> map, WarningSet set) {
@@ -510,12 +547,12 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	 * 
 	 * @param configuration		Rocket configuration
 	 * @param conditions		Flight conditions taken into account
-	 * @param map				?
+	 * @param forceMap
-	 * @param set				Set to handle 
+	 * @param warningSet			all current warnings
 	 * @return
 	 */
 	private double calculatePressureDrag(FlightConfiguration configuration, FlightConditions conditions,
-			Map<RocketComponent, AerodynamicForces> map, WarningSet warnings) {
+			Map<RocketComponent, AerodynamicForces> forceMap, WarningSet warningSet) {
 		
 		double stagnation, base, total;
 		
@@ -538,11 +575,11 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 
 				// Pressure fore drag
 				double cd = calcMap.get(c).calculatePressureDragForce(conditions, stagnation, base,
-																	  warnings);
+																	  warningSet);
 				total += cd;
 
-				if (map != null) {
+				if (forceMap != null) {
-					map.get(c).setPressureCD(cd);
+					forceMap.get(c).setPressureCD(cd);
 				}
 				
 				if(c.isCDOverridden())
@@ -562,8 +599,8 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 						cd = stagnation * area / conditions.getRefArea();
 						total += cd;
 						
-						if (map != null) {
+						if (forceMap != null) {
-							map.get(c).setPressureCD(map.get(c).getPressureCD() + cd);
+							forceMap.get(c).setPressureCD(forceMap.get(c).getPressureCD() + cd);
 						}
 					}
 				}
@@ -580,7 +617,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	 * @param configuration		Rocket configuration
 	 * @param conditions		Flight conditions taken into account
 	 * @param map				?
-	 * @param set				Set to handle 
+	 * @param warnings				all current warnings
 	 * @return
 	 */
 	private double calculateBaseDrag(FlightConfiguration configuration, FlightConditions conditions,
@@ -752,10 +789,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 		total.setPitchDampingMoment(MathUtil.sign(pitchRate) * pitchDampingMomentMagnitude);
 		total.setYawDampingMoment(MathUtil.sign(yawRate) * yawDampingMomentMagnitude);
 	}
-	
+
-	// TODO: MEDIUM: Are the rotation etc. being added correctly?  sin/cos theta?
-	
-	
 	private double getDampingMultiplier(FlightConfiguration configuration, FlightConditions conditions,
 			double cgx) {
 		if (cacheDiameter < 0) {
@@ -811,18 +845,15 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	
 	
 	private void buildCalcMap(FlightConfiguration configuration) {
-		Iterator<RocketComponent> iterator;
+		calcMap = new HashMap<>();
-		
-		calcMap = new HashMap<RocketComponent, RocketComponentCalc>();
 
+		// because this is not a per-instance iteration... this usage of 'getActiveComponents' is probably fine.
 		for (RocketComponent comp: configuration.getActiveComponents()) {
 			if (!comp.isAerodynamic())
 				continue;
-			
+
 			RocketComponentCalc calcObj = (RocketComponentCalc) Reflection.construct(BARROWMAN_PACKAGE, comp, BARROWMAN_SUFFIX, comp);
-			//String isNull = (null==calcObj?"null":"valid");
+
-			//System.err.println("    >> At component: "+c.getName() +"=="+c.getID()+". CalcObj is "+isNull);
-			
 			calcMap.put(comp, calcObj ); 
 		}
 	}

core/src/net/sf/openrocket/masscalc/CMAnalysisEntry.java

@@ -0,0 +1,40 @@
+package net.sf.openrocket.masscalc;
+
+import net.sf.openrocket.motor.Motor;
+import net.sf.openrocket.rocketcomponent.RocketComponent;
+import net.sf.openrocket.util.Coordinate;
+
+public class CMAnalysisEntry {
+
+    public CMAnalysisEntry(final Object _src) {
+        source = _src;
+        if (source instanceof RocketComponent){
+            name = ((RocketComponent)source).getName();
+        }else if( source instanceof Motor ){
+            name = ((Motor) source).getDesignation();
+        }else {
+            name = null;
+        }
+        eachMass = Double.NaN;
+        totalCM = Coordinate.NaN;
+    }
+
+    public String name;
+    public Object source;
+    public double eachMass;
+    public Coordinate totalCM;
+
+    public void updateEachMass(final double newMass) {
+        if (Double.isNaN(eachMass)) {
+            eachMass = newMass;
+        }
+    }
+
+    public void updateAverageCM(final Coordinate newCM) {
+        if (this.totalCM.isNaN()) {
+            this.totalCM = newCM;
+        } else {
+            this.totalCM = totalCM.average(newCM);
+        }
+    }
+}

core/src/net/sf/openrocket/masscalc/MassCalculation.java

@@ -1,12 +1,11 @@
 package net.sf.openrocket.masscalc;
 
 import java.util.ArrayList;
+import java.util.Map;
 
 import net.sf.openrocket.motor.Motor;
 import net.sf.openrocket.motor.MotorConfiguration;
-import net.sf.openrocket.rocketcomponent.FlightConfiguration;
+import net.sf.openrocket.rocketcomponent.*;
-import net.sf.openrocket.rocketcomponent.MotorMount;
-import net.sf.openrocket.rocketcomponent.RocketComponent;
 import net.sf.openrocket.util.Coordinate;
 import net.sf.openrocket.util.MathUtil;
 import net.sf.openrocket.util.Transformation;
@@ -73,8 +72,8 @@ public class MassCalculation {
 		}
 	}
 	
-	public MassCalculation copy( final RocketComponent _root, final Transformation _transform ){
+	public MassCalculation copy( final RocketComponent _root, final Transformation _transform){
-		return new MassCalculation( this.type, this.config, this.simulationTime, _root, _transform );
+		return new MassCalculation( this.type, this.config, this.simulationTime, _root, _transform, this.analysisMap);
 	}
 		
 	public Coordinate getCM() {
@@ -110,13 +109,17 @@ public class MassCalculation {
 		return (int) (this.centerOfMass.hashCode());
 	}
 
-	public MassCalculation( final Type _type, final FlightConfiguration _config, final double _time, final RocketComponent _root, final Transformation _transform) {
+	public MassCalculation( final Type _type, final FlightConfiguration _config, final double _time,
+							final RocketComponent _root, final Transformation _transform,
+							Map<Integer, CMAnalysisEntry> _map)
+	{
 		type = _type;
 		config = _config;
 		simulationTime = _time;
 		root = _root;
 		transform = _transform;
-		
+		analysisMap = _map;
+
 		reset();
 	}
 	
@@ -167,8 +170,10 @@ public class MassCalculation {
 	
 	// center-of-mass AND moment-of-inertia data.
 	final ArrayList<RigidBody> bodies = new ArrayList<RigidBody>();
-	
+
-	String prefix = "";		
+	String prefix = "";
+
+	Map<Integer, CMAnalysisEntry> analysisMap;
 
 	// =========== Private Instance Functions ========================
 
@@ -183,8 +188,8 @@ public class MassCalculation {
 		if( motorConfig.isEmpty() ){
 			return this;
 		}
-		
+
-		
+
 		final double mountXPosition = root.getPosition().x;
 		
 		final int instanceCount = root.getInstanceCount();
@@ -210,10 +215,10 @@ public class MassCalculation {
 			eachMass = eachMotorMass - eachCasingMass;
 			eachCMx = (eachMotorCMx*eachMotorMass - eachCasingCMx*eachCasingMass)/eachMass;
 		}
-		
+
 //		System.err.println(String.format("%-40s|Motor: %s....  Mass @%f = %.6f", prefix, motorConfig.toDescription(), simulationTime, eachMass ));
-		
+
-		
+
 		// coordinates in rocket frame; Ir, It about CoM.
 		final Coordinate clusterLocalCM = new Coordinate( mountXPosition + motorXPosition + eachCMx, 0, 0, eachMass*instanceCount);
 		
@@ -232,7 +237,17 @@ public class MassCalculation {
 		
 		final Coordinate clusterCM = transform.transform( clusterLocalCM  );
 		addMass( clusterCM );
-		
+
+		if(null != this.analysisMap) {
+			CMAnalysisEntry entry = analysisMap.get(motor.getDesignation());
+			if (null == entry){
+				entry = new CMAnalysisEntry(motor);
+				analysisMap.put(motor.getDesignation().hashCode(), entry);
+			}
+			entry.updateEachMass(eachMass);
+			entry.updateAverageCM(clusterCM);
+		}
+
 		RigidBody clusterMOI = new RigidBody( clusterCM, clusterIr, clusterIt, clusterIt );
 		addInertia( clusterMOI );
 		
@@ -273,7 +288,14 @@ public class MassCalculation {
 		// if( this.config.isComponentActive(component) ){
 		// 	System.err.println(String.format( "%s>>[%s]....", prefix, component.getName()));
 		// }
-		
+
+		if(null != analysisMap) {
+			if (this.config.isComponentActive(component) && (! analysisMap.containsKey(component.hashCode()))){
+				CMAnalysisEntry entry = new CMAnalysisEntry(component);
+				analysisMap.put(component.hashCode(), entry);
+			}
+		}
+
 		// iterate over the aggregated instances for the whole tree.
 		MassCalculation children = this.copy(component, parentTransform );
 		for( int currentInstanceNumber = 0; currentInstanceNumber < instanceCount; ++currentInstanceNumber) {
@@ -288,14 +310,14 @@ public class MassCalculation {
 
 			for (RocketComponent child : component.getChildren()) {
 				// child data, relative to rocket reference frame
-				MassCalculation eachChild = copy( child, currentTransform);
+				MassCalculation eachChild = copy(child, currentTransform);
 				
 				eachChild.prefix = prefix + "....";
 				eachChild.calculateStructure(); 
 				
 				// accumulate children's data
 				children.merge( eachChild );
-			}			
+			}
 		}
 		
 		if( MIN_MASS < children.getMass() ) {
@@ -320,6 +342,20 @@ public class MassCalculation {
 			// mass data for *this component only* in the rocket-frame
 			compCM = parentTransform.transform( compCM.add(component.getPosition()) );
 			this.addMass( compCM );
+
+			if(null != analysisMap){
+				if( component instanceof ComponentAssembly) {
+					// For ComponentAssemblies, record the _assembly_ information
+					CMAnalysisEntry entry = analysisMap.get(component.hashCode());
+					entry.updateEachMass(children.getMass() / component.getInstanceCount());
+					entry.updateAverageCM(this.centerOfMass);
+				}else{
+					// For actual components, record the mass of the component, and disregard children
+					CMAnalysisEntry entry = analysisMap.get(component.hashCode());
+					entry.updateEachMass(compCM.weight);
+					entry.updateAverageCM(compCM);
+				}
+			}
 			
 			double compIx = component.getRotationalUnitInertia() * compCM.weight;
 			double compIt = component.getLongitudinalUnitInertia() * compCM.weight;
@@ -331,7 +367,7 @@ public class MassCalculation {
 			// 	System.err.println(String.format( "%s....componentData:            %s", prefix, compCM.toPreciseString() ));
 			// }
 
-			if (component.getOverrideSubcomponents()) {				
+			if (component.getOverrideSubcomponents()) {
 				if (component.isMassOverridden()) {
 					double newMass = MathUtil.max(component.getOverrideMass(), MIN_MASS);
 					Coordinate newCM = this.getCM().setWeight( newMass );
@@ -355,29 +391,29 @@ public class MassCalculation {
 	}
 
 	MassCalculation calculateMotors() {
-	
 		final RocketComponent component = this.root;
 		final Transformation parentTransform = this.transform;
 		
 		final int instanceCount = component.getInstanceCount();
 		Coordinate[] instanceLocations = component.getInstanceLocations();
-		
+
 //		// vvv DEBUG
 //		if( this.config.isComponentActive(component) ){
 //			System.err.println(String.format( "%s[%s]....", prefix, component.getName()));
 //		}
-		
+
 		if (component.isMotorMount()) {
 			MassCalculation propellant = this.copy(component, parentTransform);
 			
 			propellant.calculateMountData();
-			
+
 			this.merge( propellant );
 
-//		    // vvv DEBUG			
+//			// vvv DEBUG
 //			if( 0 < propellant.getMass() ) {
 //				System.err.println(String.format( "%s........++ propellantData: %s", prefix, propellant.toCMDebug()));
 //			}
+
 		}
 		
 		// iterate over the aggregated instances for the whole tree.
@@ -395,7 +431,7 @@ public class MassCalculation {
 				
 				// accumulate children's data
 				children.merge( eachChild );
-			}			
+			}
 		}
 		
 		if( MIN_MASS < children.getMass() ) {
@@ -407,7 +443,7 @@ public class MassCalculation {
 //		if( this.config.isComponentActive(component) && 0 < this.getMass() ) {
 //			System.err.println(String.format( "%s....<< return assemblyData:   %s (tree @%s)", prefix, this.toCMDebug(), component.getName() ));
 //		}
-// ^^^ DEBUG
+//      // ^^^ DEBUG
 		
 		return this;
 	}
@@ -427,9 +463,8 @@ public class MassCalculation {
 			It += eachGlobal.Iyy;
 		}
 		
-		return new RigidBody( centerOfMass, Ir, It, It );	
+		return new RigidBody( centerOfMass, Ir, It, It );
 	}
 
-	
 }
 

core/src/net/sf/openrocket/masscalc/MassCalculator.java

@@ -7,10 +7,7 @@ import net.sf.openrocket.motor.Motor;
 import net.sf.openrocket.rocketcomponent.FlightConfiguration;
 import net.sf.openrocket.rocketcomponent.RocketComponent;
 import net.sf.openrocket.simulation.SimulationStatus;
-import net.sf.openrocket.util.Coordinate;
+import net.sf.openrocket.util.*;
-import net.sf.openrocket.util.MathUtil;
-import net.sf.openrocket.util.Monitorable;
-import net.sf.openrocket.util.Transformation;
 
 public class MassCalculator implements Monitorable {
 	
@@ -104,7 +101,7 @@ public class MassCalculator implements Monitorable {
 	public static RigidBody calculate( final MassCalculation.Type _type, final SimulationStatus status ){
 		final FlightConfiguration config = status.getConfiguration();
 		final double time = status.getSimulationTime();
-		MassCalculation calculation= new MassCalculation( _type, config, time, config.getRocket(), Transformation.IDENTITY);
+		MassCalculation calculation= new MassCalculation( _type, config, time, config.getRocket(), Transformation.IDENTITY, null);
 		
 		calculation.calculateAssembly();
 		RigidBody result = calculation.calculateMomentOfInertia();
@@ -112,55 +109,51 @@ public class MassCalculator implements Monitorable {
 	}
 	
 	// convenience wrapper -- use this to implicitly create a plain MassCalculation object with common parameters 
-	public static RigidBody calculate( final MassCalculation.Type _type, final FlightConfiguration _config,  double _time ){
+	public static RigidBody calculate( final MassCalculation.Type _type, final FlightConfiguration _config,  double _time){
-		MassCalculation calculation = new MassCalculation( _type, _config, _time, _config.getRocket(), Transformation.IDENTITY);
+		MassCalculation calculation = new MassCalculation( _type, _config, _time, _config.getRocket(), Transformation.IDENTITY, null);
 		calculation.calculateAssembly();
 		return calculation.calculateMomentOfInertia();
 	}
 
-	
 	/**
 	 * Compute an analysis of the per-component CG's of the provided configuration.
 	 * The returned map will contain an entry for each physical rocket component (not stages)
 	 * with its corresponding (best-effort) CG.  Overriding of subcomponents is ignored.
 	 * The CG of the entire configuration with motors is stored in the entry with the corresponding
 	 * Rocket as the key.
-	 * 
+	 *
 	 * Deprecated:
-	 * This function is fundamentally broken, because it asks for a calculation which ignores instancing.  
+	 * This function is fundamentally broken, because it asks for a calculation which ignores instancing.
 	 * This function will work with simple rockets, but will be misleading or downright wrong for others.
-	 * 
+	 *
-	 * This is a problem with using a single-typed map:  
+	 * This is a problem with using a single-typed map:
 	 * [1] multiple instances of components are not allowed, and must be merged.
 	 * [2] propellant / motor data does not have a corresponding RocketComponent.
-	 *     ( or mount-data collides with motor-data )  
+	 *     ( or mount-data collides with motor-data )
 	 *
-	 * @param configuration		the rocket configuration
+	 * @return a list of CG coordinates for every instance of this component
-	 * @return					a map from each rocket component to its corresponding CG.
 	 */
-	@Deprecated
+	public static Map<Integer,CMAnalysisEntry> getCMAnalysis(FlightConfiguration config) {
-	public Map<RocketComponent, Coordinate> getCGAnalysis(FlightConfiguration configuration) {
-		//		revalidateCache(configuration);
-		
-		Map<RocketComponent, Coordinate> map = new HashMap<RocketComponent, Coordinate>();
-		
-		Coordinate rocketCG = Coordinate.ZERO;
-		for (RocketComponent comp : configuration.getActiveComponents()) {
-			Coordinate[] cgs = comp.toAbsolute(comp.getCG());
-			Coordinate stageCG = Coordinate.NUL;
-			for (Coordinate cg : cgs) {
-				stageCG = stageCG.average(cg);
-			}
-			map.put(comp, stageCG);
-			
-			rocketCG.average( stageCG);
-		}
-		
-		map.put(configuration.getRocket(), rocketCG );
-		
-		return map;
-	}
 
+		Map<Integer,CMAnalysisEntry> analysisMap = new HashMap<>();
+
+		MassCalculation calculation = new MassCalculation(
+				MassCalculation.Type.LAUNCH,
+				config,
+				Motor.PSEUDO_TIME_LAUNCH,
+				config.getRocket(),
+				Transformation.IDENTITY,
+				analysisMap);
+
+		calculation.calculateAssembly();
+
+		CMAnalysisEntry totals = new CMAnalysisEntry(config.getRocket());
+		totals.totalCM = calculation.centerOfMass;
+		totals.eachMass = calculation.centerOfMass.weight;
+		analysisMap.put(config.getRocket().hashCode(), totals);
+
+		return analysisMap;
+	}
 	
 	////////////////// Mass property calculations  ///////////////////
 	@Override

core/src/net/sf/openrocket/rocketcomponent/FlightConfiguration.java

@@ -202,23 +202,16 @@ public class FlightConfiguration implements FlightConfigurableParameter<FlightCo
 	}
 
 	public Collection<RocketComponent> getAllComponents() {
-		Queue<RocketComponent> toProcess = new ArrayDeque<RocketComponent>();
+		List<RocketComponent> traversalOrder = new ArrayList<RocketComponent>();
-		toProcess.offer(this.rocket);
+		recurseAllComponentsDepthFirst(this.rocket,traversalOrder);
-		
+		return traversalOrder;
-		ArrayList<RocketComponent> toReturn = new ArrayList<>();
+	}
-		
+
-		while (!toProcess.isEmpty()) {
+	private void recurseAllComponentsDepthFirst(RocketComponent comp, List<RocketComponent> traversalOrder){
-			RocketComponent comp = toProcess.poll();
+		traversalOrder.add(comp);
-			
+		for( RocketComponent child : comp.getChildren()){
-			toReturn.add(comp);
+			recurseAllComponentsDepthFirst(child, traversalOrder);
-			for (RocketComponent child : comp.getChildren()) {
-				if (!(child instanceof AxialStage)) {
-					toProcess.offer(child);
-				}
-			}
 		}
-		
-		return toReturn;
 	}
 
 	/** Returns all the components on core stages (i.e. centerline)
@@ -401,10 +394,10 @@ public class FlightConfiguration implements FlightConfigurableParameter<FlightCo
 	}
 	
 	private void updateStages() {
-        if (this.rocket.getStageCount() == this.stages.size()) {
+		if (this.rocket.getStageCount() == this.stages.size()) {
-            return;
+			return;
-        }
+		}
-	                		
+
 		this.stages.clear();
 		for (AxialStage curStage : this.rocket.getStageList()) {
 			

core/test/net/sf/openrocket/aerodynamics/BarrowmanCalculatorTest.java

@@ -341,12 +341,9 @@ public class BarrowmanCalculatorTest {
 		
 		final Coordinate cpNoPods = calcNoPods.getCP(configNoPods, conditionsNoPods, warningsNoPods);
 		final Coordinate cpPods = calcPods.getCP(configPods, conditionsPods, warningsPods);
-		System.out.printf("with pods %s\n", cpPods.toString());
-		System.out.printf("without pods %s\n", cpNoPods.toString());
 		assertEquals(" Alpha III With Pods rocket cp x value is incorrect:", cpNoPods.x - 0.002788761352, cpPods.x, EPSILON);
 		assertEquals(" Alpha III With Pods rocket cp y value is incorrect:", cpNoPods.y, cpPods.y, EPSILON);
 		assertEquals(" Alpha III With Pods rocket cp z value is incorrect:", cpNoPods.z, cpPods.z, EPSILON);
 		assertEquals(" Alpha III With Pods rocket CNa value is incorrect:", cpPods.weight, cpNoPods.weight - 3.91572, EPSILON);
 	}
-			
 }

swing/src/net/sf/openrocket/gui/dialogs/ComponentAnalysisDialog.java

@@ -19,7 +19,6 @@ import java.util.Vector;
 
 import javax.swing.BorderFactory;
 import javax.swing.JButton;
-import javax.swing.JComboBox;
 import javax.swing.JDialog;
 import javax.swing.JFrame;
 import javax.swing.JLabel;
@@ -54,21 +53,22 @@ import net.sf.openrocket.gui.components.UnitSelector;
 import net.sf.openrocket.gui.scalefigure.RocketPanel;
 import net.sf.openrocket.gui.util.GUIUtil;
 import net.sf.openrocket.l10n.Translator;
+import net.sf.openrocket.masscalc.CMAnalysisEntry;
 import net.sf.openrocket.masscalc.MassCalculator;
 import net.sf.openrocket.motor.MotorConfiguration;
-import net.sf.openrocket.rocketcomponent.AxialStage;
+import net.sf.openrocket.rocketcomponent.*;
-import net.sf.openrocket.rocketcomponent.FinSet;
-import net.sf.openrocket.rocketcomponent.FlightConfiguration;
-import net.sf.openrocket.rocketcomponent.Rocket;
-import net.sf.openrocket.rocketcomponent.RocketComponent;
 import net.sf.openrocket.startup.Application;
 import net.sf.openrocket.unit.Unit;
 import net.sf.openrocket.unit.UnitGroup;
 import net.sf.openrocket.util.Coordinate;
 import net.sf.openrocket.util.MathUtil;
 import net.sf.openrocket.util.StateChangeListener;
+import org.slf4j.Logger;
+import org.slf4j.LoggerFactory;
 
 public class ComponentAnalysisDialog extends JDialog implements StateChangeListener {
+	private static final Logger log = LoggerFactory.getLogger(ComponentAnalysisDialog.class);
+
 	private static final long serialVersionUID = 9131240570600307935L;
 	private static ComponentAnalysisDialog singletonDialog = null;
 	private static final Translator trans = Application.getTranslator();
@@ -80,18 +80,16 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 	private final JToggleButton worstToggle;
 	private boolean fakeChange = false;
 	private AerodynamicCalculator aerodynamicCalculator;
-	private final MassCalculator massCalculator = new MassCalculator();
 
-	private final ColumnTableModel cpTableModel;
+	private final ColumnTableModel longitudeStabilityTableModel;
 	private final ColumnTableModel dragTableModel;
 	private final ColumnTableModel rollTableModel;
 
 	private final JList<Object> warningList;
 
 
-	private final List<Object[]> cgData = new ArrayList<Object[]>();
+	private final List<LongitudinalStabilityRow> stabData = new ArrayList<>();
 	private final List<AerodynamicForces> dragData = new ArrayList<AerodynamicForces>();
-	private double totalCD = 0;
 	private final List<AerodynamicForces> rollData = new ArrayList<AerodynamicForces>();
 
 
@@ -186,69 +184,59 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 		panel.add(tabbedPane, "spanx, growx, growy");
 
 
-		// Create the CP data table
+		// Create the Longitudinal Stability (CM vs CP) data table
-		cpTableModel = new ColumnTableModel(
+		longitudeStabilityTableModel = new ColumnTableModel(
 
 				//// Component
 				new Column(trans.get("componentanalysisdlg.TabStability.Col.Component")) {
 					@Override
 					public Object getValueAt(int row) {
-						Object c = cgData.get(row)[0];
+						Object c = stabData.get(row).name;
-						if (c instanceof Rocket) {
-							return trans.get("componentanalysisdlg.TOTAL");
-						}
 						return c.toString();
 					}
-					
+
 					@Override
 					public int getDefaultWidth() {
 						return 200;
 					}
 				},
-				new Column(trans.get("componentanalysisdlg.TabStability.Col.CG") + " / " + UnitGroup.UNITS_LENGTH.getDefaultUnit().getUnit()) {
+				 // would be per-instance mass
-					private Unit unit = UnitGroup.UNITS_LENGTH.getDefaultUnit();
+				new Column(trans.get("componentanalysisdlg.TabStability.Col.EachMass") + " (" + UnitGroup.UNITS_MASS.getDefaultUnit().getUnit() + ")") {
-					
+					final private Unit unit = UnitGroup.UNITS_MASS.getDefaultUnit();
+
 					@Override
 					public Object getValueAt(int row) {
-						Coordinate cg = (Coordinate) cgData.get(row)[1];
+						return unit.toString(stabData.get(row).eachMass);
-						if ( cg == null ) {
-							return null;
-						}
-						return unit.toString(cg.x);
 					}
 				},
-				new Column(trans.get("componentanalysisdlg.TabStability.Col.Mass") + " / " + UnitGroup.UNITS_MASS.getDefaultUnit().getUnit()) {
+				new Column(trans.get("componentanalysisdlg.TabStability.Col.AllMass") + " (" + UnitGroup.UNITS_MASS.getDefaultUnit().getUnit() + ")") {
-					private Unit unit = UnitGroup.UNITS_MASS.getDefaultUnit();
+					final private Unit unit = UnitGroup.UNITS_MASS.getDefaultUnit();
-					
+
 					@Override
 					public Object getValueAt(int row) {
-						Coordinate cg = (Coordinate) cgData.get(row)[1];
+						return unit.toString(stabData.get(row).cm.weight);
-						if ( cg == null ) {
-							return null;
-						}
-						return unit.toString(cg.weight);
 					}
 				},
-				new Column(trans.get("componentanalysisdlg.TabStability.Col.CP") + " / " + UnitGroup.UNITS_LENGTH.getDefaultUnit().getUnit()) {
+				new Column(trans.get("componentanalysisdlg.TabStability.Col.CG") + " (" + UnitGroup.UNITS_LENGTH.getDefaultUnit().getUnit() + ")") {
-					private Unit unit = UnitGroup.UNITS_LENGTH.getDefaultUnit();
+					final private Unit unit = UnitGroup.UNITS_LENGTH.getDefaultUnit();
 					
 					@Override
 					public Object getValueAt(int row) {
-						AerodynamicForces forces = (AerodynamicForces) cgData.get(row)[2];
+						return unit.toString(stabData.get(row).cm.x);
-						if ( forces == null ) {
+					}
-							return null;
+				},
-						}
+				new Column(trans.get("componentanalysisdlg.TabStability.Col.CP") + " (" + UnitGroup.UNITS_LENGTH.getDefaultUnit().getUnit() + ")") {
-						return unit.toString(forces.getCP().x);
+					final private Unit unit = UnitGroup.UNITS_LENGTH.getDefaultUnit();
+					
+					@Override
+					public Object getValueAt(int row) {
+						return NOUNIT.toString(stabData.get(row).cpx);
 					}
 				},
 				new Column("<html>C<sub>N<sub>" + ALPHA + "</sub></sub>") {
 					@Override
 					public Object getValueAt(int row) {
-						AerodynamicForces forces = (AerodynamicForces) cgData.get(row)[2];
+						return NOUNIT.toString(stabData.get(row).cna);
-						if ( forces == null ) {
-							return null;
-						}
-						return NOUNIT.toString(forces.getCP().weight);
 					}
 				}
 	
@@ -261,15 +249,15 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 
 			@Override
 			public int getRowCount() {
-				return cgData.size();
+				return stabData.size();
 			}
 		};
 
-		table = new ColumnTable(cpTableModel);
+		table = new ColumnTable(longitudeStabilityTableModel);
 		table.setSelectionMode(ListSelectionModel.SINGLE_SELECTION);
 		table.setSelectionBackground(Color.LIGHT_GRAY);
 		table.setSelectionForeground(Color.BLACK);
-		cpTableModel.setColumnWidths(table.getColumnModel());
+		longitudeStabilityTableModel.setColumnWidths(table.getColumnModel());
 
 		table.setDefaultRenderer(Object.class, new CustomCellRenderer());
 		//		table.setShowHorizontalLines(false);
@@ -425,8 +413,6 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 
 
 
-
-
 		// Add the data updater to listen to changes in aoa and theta
 		mach.addChangeListener(this);
 		theta.addChangeListener(this);
@@ -534,80 +520,97 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 			}
 		}
 
-		Map<RocketComponent, AerodynamicForces> aeroData =
+		// key is the comp.hashCode() or motor.getDesignation().hashCode()
-				aerodynamicCalculator.getForceAnalysis(configuration, conditions, set);
+		Map<Integer, CMAnalysisEntry> cmMap= MassCalculator.getCMAnalysis(configuration);
-		Map<RocketComponent, Coordinate> massData =
-				massCalculator.getCGAnalysis(configuration);
 
+		Map<RocketComponent, AerodynamicForces> aeroData = aerodynamicCalculator.getForceAnalysis(configuration, conditions, set);
 
-		cgData.clear();
+		stabData.clear();
 		dragData.clear();
 		rollData.clear();
-		for (RocketComponent c : configuration.getActiveComponents()) {
-			if ( c instanceof AxialStage ) {
-				continue;
-			}
-			Object[] data = new Object[3];
-			cgData.add(data);
-			data[0] = c;
 
-			Coordinate cg = massData.get(c);
+		for(final RocketComponent comp: configuration.getAllComponents()) {
-			data[1] = cg;
+			// // this is actually redundant, because the analysis will not contain inactive stages.
-			
+			// if (!configuration.isComponentActive(comp)) {
-			forces = aeroData.get(c);
+			// 	continue;
-			if (forces == null) {
+			// }
+
+			CMAnalysisEntry cmEntry = cmMap.get(comp.hashCode());
+			if (null == cmEntry) {
+				log.warn("Could not find massData entry for component: " + comp.getName());
 				continue;
 			}
-			if (forces.getCP() != null) {
+
-				data[2] = forces;
+			if ((comp instanceof ComponentAssembly) && !(comp instanceof Rocket)){
+				continue;
 			}
-			
+
+			LongitudinalStabilityRow row = new LongitudinalStabilityRow(cmEntry.name, cmEntry.source);
+			stabData.add(row);
+
+			row.source = cmEntry.source;
+			row.eachMass = cmEntry.eachMass;
+			row.cm = cmEntry.totalCM;
+
+			forces = aeroData.get(comp);
+			if (forces == null) {
+				// DEBUG / trace level
+				System.err.println("Could not find aeroData entry for component: " + comp.getName());
+				row.cpx = 0.0;
+				row.cna = 0.0;
+				continue;
+			}
+
+//			System.err.println(String.format("        .CP = %s", forces.getCP()));
+			if (forces.getCP() != null) {
+				row.cpx = forces.getCP().x;
+				row.cna = forces.getCNa();
+			}
+
+//			System.err.println(String.format("        .CD = %s", forces.getCD()));
 			if (!Double.isNaN(forces.getCD())) {
 				dragData.add(forces);
 			}
-			if (c instanceof FinSet) {
+
+			if (comp instanceof FinSet) {
 				rollData.add(forces);
 			}
+			// // We _would_ check this, except TubeFinSet doesn't implement cant angles... so they can't impart any roll torque
+			// // If this is ever implemented, uncomment this block:
+			// else if(comp instanceof TubeFinSet){
+			// 	rollData.add(forces)
+			// }
 		}
 
-		for ( MotorConfiguration motorConfig : configuration.getActiveMotors()) {
+		for(final MotorConfiguration config: configuration.getActiveMotors()) {
-		
+			CMAnalysisEntry cmEntry = cmMap.get(config.getMotor().getDesignation());
-			Object [] data = new Object[3];
+			if (null == cmEntry) {
-			cgData.add(data);
+				continue;
-			
+			}
-			data[0] = motorConfig.getMotor().getDesignation();
+
-			data[1] = motorConfig.getMotor().getLaunchMass(); 
+			LongitudinalStabilityRow row = new LongitudinalStabilityRow(cmEntry.name, cmEntry.source);
-		}
+			stabData.add(row);
-		
+
-		forces = aeroData.get(rkt);
+			row.source = cmEntry.source;
-		if (forces != null) {
+			row.eachMass = cmEntry.eachMass;
-			Object[] data = new Object[3];
+			row.cm = cmEntry.totalCM;
-			cgData.add(data);
+			row.cpx = 0.0;
-			data[0] = rkt;
+			row.cna = 0.0;
-			data[1] = massData.get(rkt);
-			data[2] = forces;
-			dragData.add(forces);
-			rollData.add(forces);
-			totalCD = forces.getCD();
-		} else {
-			totalCD = 0;
 		}
 
 		// Set warnings
 		if (set.isEmpty()) {
-			warningList.setListData(new String[] {
+			warningList.setListData(new String[] {trans.get("componentanalysisdlg.noWarnings")
-					trans.get("componentanalysisdlg.noWarnings")
 			});
 		} else {
 			warningList.setListData(new Vector<Warning>(set));
 		}
 
-		cpTableModel.fireTableDataChanged();
+		longitudeStabilityTableModel.fireTableDataChanged();
 		dragTableModel.fireTableDataChanged();
 		rollTableModel.fireTableDataChanged();
 	}
 
-
 	private class CustomCellRenderer extends JLabel implements TableCellRenderer {
 		/**
 		 * 
@@ -628,10 +631,10 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 
 			this.setText(value == null ? null : value.toString());
 
-			if ((row < 0) || (row >= cgData.size()))
+			if ((row < 0) || (row >= stabData.size()))
 				return this;
 
-			if (cgData.get(row)[0] instanceof Rocket) {
+			if ( 0 == row ) {
 				this.setFont(boldFont);
 			} else {
 				this.setFont(normalFont);
@@ -662,6 +665,7 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 				boolean isSelected, boolean hasFocus, int row, int column) {
 
 			if (value instanceof Double) {
+				final double totalCD = dragData.get(0).getCD();
 
 				// A drag coefficient
 				double cd = (Double) value;
@@ -698,6 +702,25 @@ public class ComponentAnalysisDialog extends JDialog implements StateChangeListe
 		}
 	}
 
+	private class LongitudinalStabilityRow {
+
+		public String name;
+		public Object source;
+		public double eachMass;
+		public Coordinate cm;
+		public double cpx;
+		public double cna;
+
+		public LongitudinalStabilityRow(final String _name, final Object _source){
+			name = _name;
+			source = _source;
+			eachMass = Double.NaN;
+			cm = Coordinate.NaN;
+			cpx = Double.NaN;
+			cna = Double.NaN;
+		}
+
+	}
 
 	/////////  Singleton implementation
 

swing/src/net/sf/openrocket/gui/main/BasicFrame.java

@@ -682,19 +682,18 @@ public class BasicFrame extends JFrame {
 		menubar.add(menu);
 
 
-//      TODO: reimplement this
+		//// Component analysis
-//		//// Component analysis
+		item = new JMenuItem(trans.get("main.menu.analyze.componentAnalysis"), KeyEvent.VK_C);
-//		item = new JMenuItem(trans.get("main.menu.analyze.componentAnalysis"), KeyEvent.VK_C);
+		//// Analyze the rocket components separately
-//		//// Analyze the rocket components separately
+		item.getAccessibleContext().setAccessibleDescription(trans.get("main.menu.analyze.componentAnalysis.desc"));
-//		item.getAccessibleContext().setAccessibleDescription(trans.get("main.menu.analyze.componentAnalysis.desc"));
+		item.addActionListener(new ActionListener() {
-//		item.addActionListener(new ActionListener() {
+			@Override
-//			@Override
+			public void actionPerformed(ActionEvent e) {
-//			public void actionPerformed(ActionEvent e) {
+				log.info(Markers.USER_MARKER, "Component analysis selected");
-//				log.info(Markers.USER_MARKER, "Component analysis selected");
+				ComponentAnalysisDialog.showDialog(rocketpanel);
-//				ComponentAnalysisDialog.showDialog(rocketpanel);
+			}
-//			}
+		});
-//		});
+		menu.add(item);
-//		menu.add(item);
 
 // TODO: reimplement this dialog
 //		//// Optimize