LVD:

1) Added an initial implementation of Graphical Analysis for LVD.
2) Cleaned up a few files with incorrect header comments here and there.

helper_methods/ksptot_ma/graph_analysis/ma_getDepVarValueUnit.m

@@ -237,5 +237,4 @@
             depVarValue = ma_OutboundHyperVelVectTask(subLog(i,:), 'mag', celBodyData);
             depVarUnit = 'km/s';
     end
-end
-
+end

helper_methods/ksptot_ma/graph_analysis/ma_getGraphAnalysisTaskList.m

@@ -72,5 +72,4 @@
     taskList{end+1} = 'Hyperbolic Velocity Magnitude';
 
     taskList = setdiff(taskList,excludeList);
-end
-
+end

helper_methods/ksptot_ma/graph_analysis/tasks/ma_TimeTask.m

@@ -1,5 +1,5 @@
 function datapt = ma_TimeTask(stateLogEntry, subTask, celBodyData)
-%ma_GAVectorElementsTask Summary of this function goes here
+%ma_TimeTask Summary of this function goes here
 %   Detailed explanation goes here
 
     switch subTask

helper_methods/ksptot_ma/gui/substituteDefaultPropNamesWithCustomNamesInDepVarListbox.m

@@ -1,6 +1,6 @@
-function substituteDefaultPropNamesWithCustomNamesInDepVarListbox(hDepVarListbox, maData)
+function substituteDefaultPropNamesWithCustomNamesInDepVarListbox(hDepVarListbox, propNames)
     vars = get(hDepVarListbox,'String');
-    propNames = maData.spacecraft.propellant.names;
+%     propNames = maData.spacecraft.propellant.names;
     defaultNames = {'Liquid Fuel/Ox Mass','Monopropellant Mass','Xenon Mass'};
 
     for(i=1:length(vars)) %#ok<*NO4LP>

helper_methods/ksptot_ma/launch_vehicle_designer/classes/@LvdData/LvdData.m

@@ -26,7 +26,7 @@
         end
     end
 
-    methods
+    methods        
         function initialState = get.initialState(obj)
             initialState = obj.initStateModel.getInitialStateLogEntry();
         end
@@ -52,7 +52,7 @@
         end
     end
 
-    methods(Static)
+    methods(Static)        
         function lvdData = getEmptyLvdData()
             lvdData = LvdData();
             lvdData.ksptotVer = getKSPTOTVersionNumStr();

helper_methods/ksptot_ma/launch_vehicle_designer/classes/Events/@LaunchVehicleScript/LaunchVehicleScript.m

@@ -8,7 +8,7 @@
         lvdData LvdData
     end
 
-    properties(Access=private)
+    properties%(Access=private)
         simDriver LaunchVehicleSimulationDriver
     end
 
@@ -170,12 +170,15 @@ function moveEvtAtIndexUp(obj, ind)
 %             figure(123);
 %             subplot(3,1,1)
 %             plot(time,totalMass);
+%             grid on;
 %             
 %             subplot(3,1,2)
 %             plot(time,pitchActual);
+%             grid on;
 %             
 %             subplot(3,1,3)
 %             plot(time,angOfAttackActual);
+%             grid on;
         end
     end
 end

helper_methods/ksptot_ma/launch_vehicle_designer/classes/StateLog/@LaunchVehicleAttitudeState/LaunchVehicleAttitudeState.m

@@ -17,6 +17,8 @@
             bodyZ = obj.dcm(:,3);
 
             [rollAngle, pitchAngle, yawAngle] = computeEulerAnglesFromInertialBodyAxes(ut, rVect, vVect, bodyInfo, bodyX, bodyY, bodyZ);
+            rollAngle = AngleZero2Pi(rollAngle);
+            yawAngle = AngleZero2Pi(yawAngle);
         end
 
         function [bankAng,angOfAttack,angOfSideslip] = getAeroAngles(obj, rVect, vVect)
@@ -25,6 +27,8 @@
             bodyZ = obj.dcm(:,3);
 
             [bankAng,angOfAttack,angOfSideslip] = computeAeroAnglesFromBodyAxes(rVect, vVect, bodyX, bodyY, bodyZ);
+            bankAng = AngleZero2Pi(bankAng);
+            angOfSideslip = AngleZero2Pi(angOfSideslip);
         end
 
         function newAttState = deepCopy(obj)

helper_methods/ksptot_ma/launch_vehicle_designer/classes/StateLog/@LaunchVehicleStateLog/LaunchVehicleStateLog.m

@@ -30,5 +30,9 @@ function clearStateLog(obj)
             subStateLog = obj.entries([obj.entries.event] == event);
             stateLogEntry = subStateLog(end);
         end
+
+        function subLog = getStateLogEntriesBetweenTimes(obj, t1, t2)
+            subLog = obj.entries([obj.entries.time] >= t1 & [obj.entries.time] <= t2);
+        end
     end
 end

helper_methods/ksptot_ma/launch_vehicle_designer/process_data/lvd_SteeringAngleTask.m

@@ -0,0 +1,28 @@
+function datapt = lvd_SteeringAngleTask(stateLogEntry, subTask)
+%lvd_SteeringAngleTask Summary of this function goes here
+%   Detailed explanation goes here
+
+    ut = stateLogEntry.time;
+    rVect = stateLogEntry.position;
+    vVect = stateLogEntry.velocity;
+    bodyInfo = stateLogEntry.centralBody;
+
+    [rollAngle, pitchAngle, yawAngle] =  stateLogEntry.attitude.getEulerAngles(ut, rVect, vVect, bodyInfo);
+    [bankAng,angOfAttack,angOfSideslip] =  stateLogEntry.attitude.getAeroAngles(rVect, vVect);
+
+    switch subTask
+        case 'roll'
+            datapt = rad2deg(rollAngle);
+        case 'pitch'
+            datapt = rad2deg(pitchAngle);
+        case 'yaw'
+            datapt = rad2deg(yawAngle);
+        case 'bank'
+            datapt = rad2deg(bankAng);
+        case 'angleOfAttack'
+            datapt = rad2deg(angOfAttack);
+        case 'sideslip'
+            datapt = rad2deg(angOfSideslip);
+
+    end
+end

helper_methods/ksptot_ma/launch_vehicle_designer/process_data/lvd_getDepVarValueUnit.m

@@ -0,0 +1,50 @@
+function [depVarValue, depVarUnit, taskStr, refBodyInfo] = lvd_getDepVarValueUnit(i, subLog, taskStr, refBodyId, celBodyData, onlyReturnTaskStr)
+%lvd_getDepVarValueUnit Summary of this function goes here
+%   Detailed explanation goes here
+
+    if(~isempty(refBodyId))
+        refBodyInfo = getBodyInfoByNumber(refBodyId, celBodyData);
+    else
+        refBodyInfo = [];
+    end
+
+%     if(~isempty(oscId))
+%         otherSC = getOtherSCInfoByID(maData, oscId);
+%     else
+%         otherSC = [];
+%     end
+%     
+%     if(~isempty(stnId))
+%         station = getStationInfoByID(maData, stnId);
+%     else
+%         station = [];
+%     end
+
+    if(onlyReturnTaskStr == true)
+        depVarValue = NaN;
+        depVarUnit = NaN;
+
+        return;
+    end
+
+    switch taskStr
+        case 'Yaw Angle'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'yaw');
+            depVarUnit = 'deg';
+        case 'Pitch Angle'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'pitch');
+            depVarUnit = 'deg';
+        case 'Roll Angle'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'roll');
+            depVarUnit = 'deg';
+        case 'Bank Angle'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'bank');
+            depVarUnit = 'deg';
+        case 'Angle of Attack'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'angleOfAttack');
+            depVarUnit = 'deg';
+        case 'SideSlip Angle'
+            depVarValue = lvd_SteeringAngleTask(subLog(i), 'sideslip');
+            depVarUnit = 'deg';
+    end
+end

helper_methods/ksptot_ma/launch_vehicle_designer/process_data/lvd_getGraphAnalysisTaskList.m

@@ -0,0 +1,14 @@
+function [taskList] = lvd_getGraphAnalysisTaskList(excludeList)
+%ma_getGraphAnalysisTaskList Summary of this function goes here
+%   Detailed explanation goes here
+    taskList = ma_getGraphAnalysisTaskList(excludeList);
+
+    taskList{end+1} = 'Yaw Angle';
+    taskList{end+1} = 'Pitch Angle';
+    taskList{end+1} = 'Roll Angle';
+    taskList{end+1} = 'Bank Angle';
+    taskList{end+1} = 'Angle of Attack';
+    taskList{end+1} = 'SideSlip Angle';
+
+    taskList = setdiff(taskList,excludeList);
+end

helper_methods/ksptot_ma/misc/getStationInfoByID.m

@@ -1,5 +1,5 @@
 function [stationInfo] = getStationInfoByID(maData, stationID)
-%getOtherSCInfoByID Summary of this function goes here
+%getStationInfoByID Summary of this function goes here
 %   Detailed explanation goes here
 
     stationInfo = [];