public int ExportSweep(CelestialBody body, double pitch, int flapSetting, bool spoilers)
{
if (!IsReady())
{
return(0);
}
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
StaticAnalysisExportFile exportdata = new StaticAnalysisExportFile();
InstantConditionSimInput input = new InstantConditionSimInput(0, 0, 0, 0, 0, 0, FlightEnv.NewDefaultVal(body), pitch, flapSetting, spoilers);
InstantConditionSimOutput output;
Vector3d centerofmass = _instantCondition.GetCoM();
// Loop through each combination (two dimensions).
foreach (float mach in exportdata.MachNumberList)
{
input.fltenv.MachNumber = mach;
input.alpha = 0; // zero is used as a neutral value for the reset
_instantCondition.ResetClCdCmSteady(centerofmass, input); // reset old results (particularly cossweep) that may not reflect the current mach number
foreach (float aoadeg in exportdata.AoADegreeList)
{
input.alpha = aoadeg;
_instantCondition.GetClCdCmSteady(input, out output, true, true);
exportdata.AddDatapoint(mach, aoadeg, output.Cl, output.Cd, output.Cm);
}
}
exportdata.Export();
return(exportdata.DataCount);
}
public void LateUpdate()
{
FARAeroUtil.ResetEditorParts();
FARBaseAerodynamics.GlobalCoLReady = false;
if (EditorLogic.fetch)
{
if (editorGUI == null)
{
editorGUI = new FAREditorGUI();
//editorGUI.LoadGUIParameters();
editorGUI.RestartCtrlGUI();
}
if (EditorLogic.startPod != null)
{
var editorShip = FARAeroUtil.AllEditorParts;
if (FARAeroUtil.EditorAboutToAttach() && count++ >= 10)
{
EditorPartsChanged = true;
count = 0;
}
if (part_count_all != editorShip.Count || part_count_ship != EditorLogic.SortedShipList.Count || EditorPartsChanged)
{
FindPartsWithoutFARModel(editorShip);
foreach (Part p in editorShip)
{
foreach (PartModule m in p.Modules)
{
if (m is FARBaseAerodynamics)
{
(m as FARBaseAerodynamics).ClearShielding();
}
}
}
foreach (Part p in editorShip)
{
foreach (PartModule m in p.Modules)
{
if (m is FARPartModule)
{
(m as FARPartModule).ForceOnVesselPartsChange();
}
}
}
part_count_all = editorShip.Count;
part_count_ship = EditorLogic.SortedShipList.Count;
EditorPartsChanged = false;
}
}
}
}
public void LateUpdate()
{
if (!CompatibilityChecker.IsAllCompatible())
{
return;
}
FARAeroUtil.ResetEditorParts();
FARBaseAerodynamics.GlobalCoLReady = false;
if (EditorLogic.fetch)
{
if (editorGUI == null)
{
editorGUI = new FAREditorGUI();
//editorGUI.LoadGUIParameters();
editorGUI.RestartCtrlGUI();
GameEvents.onEditorUndo.Add(editorGUI.ResetAll);
GameEvents.onEditorRedo.Add(editorGUI.ResetAll);
}
if (EditorLogic.RootPart != null)
{
editorShip = FARAeroUtil.AllEditorParts;
if (buttonsNeedInitializing)
{
InitializeButtons();
}
/*if (EditorLogic.RootPart != lastRootPart)
* {
* lastRootPart = EditorLogic.RootPart;
* EditorPartsChanged = true;
* }*/
if (FARAeroUtil.EditorAboutToAttach() && count++ >= 20)
{
EditorPartsChanged = true;
count = 0;
}
if (part_count_all != editorShip.Count || part_count_ship != EditorLogic.SortedShipList.Count || EditorPartsChanged)
{
UpdateEditorShipModules();
}
}
else if (!buttonsNeedInitializing)
{
DestroyButtons();
}
}
}
public GraphData MachNumberSweep(
double aoAdegrees,
double pitch,
double lowerBound,
double upperBound,
int numPoints,
int flapSetting,
bool spoilers,
CelestialBody body
)
{
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
var ClValues = new double[numPoints];
var CdValues = new double[numPoints];
var CmValues = new double[numPoints];
var LDValues = new double[numPoints];
var AlphaValues = new double[numPoints];
var input = new InstantConditionSimInput(aoAdegrees, 0, 0, 0, 0, 0, 0, pitch, flapSetting, spoilers);
for (int i = 0; i < numPoints; i++)
{
input.machNumber = i / (double)numPoints * (upperBound - lowerBound) + lowerBound;
if (input.machNumber.NearlyEqual(0))
{
input.machNumber = 0.001;
}
_instantCondition.GetClCdCmSteady(input, out InstantConditionSimOutput output, i == 0);
AlphaValues[i] = input.machNumber;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
var data = new GraphData {
xValues = AlphaValues
};
data.AddData(ClValues, FARConfig.GUIColors.ClColor, Localizer.Format("FARAbbrevCl"), true);
data.AddData(CdValues, FARConfig.GUIColors.CdColor, Localizer.Format("FARAbbrevCd"), true);
data.AddData(CmValues, FARConfig.GUIColors.CmColor, Localizer.Format("FARAbbrevCm"), true);
data.AddData(LDValues, FARConfig.GUIColors.LdColor, Localizer.Format("FARAbbrevL_D"), true);
return(data);
}
private void ResetEditorEvent(ShipConstruct construct)
{
FARAeroUtil.ResetEditorParts();
if (EditorLogic.RootPart != null)
{
List <Part> partsList = EditorLogic.SortedShipList;
for (int i = 0; i < partsList.Count; i++)
{
UpdateGeometryModule(partsList[i]);
}
}
RequestUpdateVoxel();
}
private void ResetEditorEvent(ShipConstruct construct)
{
FARAeroUtil.ResetEditorParts(); // Rodhern: Partial fix to https://github.com/ferram4/Ferram-Aerospace-Research/issues/177 .
if (EditorLogic.RootPart != null)
{
List <Part> partsList = EditorLogic.SortedShipList;
for (int i = 0; i < partsList.Count; i++)
{
UpdateGeometryModule(partsList[i]);
}
}
RequestUpdateVoxel();
}
public GraphData MachNumberSweep(double aoAdegrees, double pitch, double lowerBound, double upperBound, int numPoints, int flapSetting, bool spoilers, CelestialBody body)
{
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
double[] ClValues = new double[(int)numPoints];
double[] CdValues = new double[(int)numPoints];
double[] CmValues = new double[(int)numPoints];
double[] LDValues = new double[(int)numPoints];
double[] AlphaValues = new double[(int)numPoints];
InstantConditionSimInput input = new InstantConditionSimInput(aoAdegrees, 0, 0, 0, 0, 0, FlightEnv.NewDefaultVal(body), pitch, flapSetting, spoilers);
for (int i = 0; i < numPoints; i++)
{
input.fltenv.MachNumber = lowerBound + (upperBound - lowerBound) * (i == 0? 0 : i / (numPoints - 1.0));
if (input.fltenv.MachNumber < 1E-3)
{
input.fltenv.MachNumber = 1E-3;
}
InstantConditionSimOutput output;
_instantCondition.GetClCdCmSteady(input, out output, i == 0, false);
AlphaValues[i] = input.fltenv.MachNumber;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
GraphData data = new GraphData();
data.xValues = AlphaValues;
data.AddData(ClValues, GUIColors.GetColor(0), Localizer.Format("FARAbbrevCl"), true);
data.AddData(CdValues, GUIColors.GetColor(1), Localizer.Format("FARAbbrevCd"), true);
data.AddData(CmValues, GUIColors.GetColor(2), Localizer.Format("FARAbbrevCm"), true);
data.AddData(LDValues, GUIColors.GetColor(3), Localizer.Format("FARAbbrevL_D"), true);
data.exportdata.AddSizeVariables(_instantCondition, pitch, flapSetting, spoilers);
data.exportdata.AddMachSweepXVariable(aoAdegrees, AlphaValues);
data.exportdata.AddYVariables(data);
return(data);
}
public GraphData MachNumberSweep(double aoAdegrees, double pitch, double lowerBound, double upperBound, int numPoints, int flapSetting, bool spoilers, CelestialBody body)
{
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
double[] ClValues = new double[(int)numPoints];
double[] CdValues = new double[(int)numPoints];
double[] CmValues = new double[(int)numPoints];
double[] LDValues = new double[(int)numPoints];
double[] AlphaValues = new double[(int)numPoints];
InstantConditionSimInput input = new InstantConditionSimInput(aoAdegrees, 0, 0, 0, 0, 0, 0, pitch, flapSetting, spoilers);
for (int i = 0; i < numPoints; i++)
{
input.machNumber = i / (double)numPoints * (upperBound - lowerBound) + lowerBound;
if (input.machNumber == 0)
{
input.machNumber = 0.001;
}
InstantConditionSimOutput output;
_instantCondition.GetClCdCmSteady(input, out output, i == 0);
AlphaValues[i] = input.machNumber;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
GraphData data = new GraphData();
data.xValues = AlphaValues;
data.AddData(ClValues, GUIColors.GetColor(0), "Cl", true);
data.AddData(CdValues, GUIColors.GetColor(1), "Cd", true);
data.AddData(CmValues, GUIColors.GetColor(2), "Cm", true);
data.AddData(LDValues, GUIColors.GetColor(3), "L/D", true);
return(data);
}
public GraphData AngleOfAttackSweep(double machNumber, double pitch, double lowerBound, double upperBound, int numPoints, int flapSetting, bool spoilers, CelestialBody body)
{
if (machNumber == 0)
{
machNumber = 0.001;
}
InstantConditionSimInput input = new InstantConditionSimInput(0, 0, 0, 0, 0, 0, machNumber, pitch, flapSetting, spoilers);
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
double[] ClValues = new double[(int)numPoints];
double[] CdValues = new double[(int)numPoints];
double[] CmValues = new double[(int)numPoints];
double[] LDValues = new double[(int)numPoints];
double[] AlphaValues = new double[(int)numPoints];
double[] ClValues2 = new double[(int)numPoints];
double[] CdValues2 = new double[(int)numPoints];
double[] CmValues2 = new double[(int)numPoints];
double[] LDValues2 = new double[(int)numPoints];
for (int i = 0; i < 2 * numPoints; i++)
{
double angle = 0;
if (i < numPoints)
{
angle = i / (double)numPoints * (upperBound - lowerBound) + lowerBound;
}
else
{
angle = (i - (double)numPoints + 1) / (double)numPoints * (lowerBound - upperBound) + upperBound;
}
input.alpha = angle;
InstantConditionSimOutput output;
_instantCondition.GetClCdCmSteady(input, out output, i == 0);
// MonoBehaviour.print("Cl: " + Cl + " Cd: " + Cd);
if (i < numPoints)
{
AlphaValues[i] = angle;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
else
{
ClValues2[numPoints * 2 - 1 - i] = output.Cl;
CdValues2[numPoints * 2 - 1 - i] = output.Cd;
CmValues2[numPoints * 2 - 1 - i] = output.Cm;
LDValues2[numPoints * 2 - 1 - i] = output.Cl * 0.1 / output.Cd;
}
}
GraphData data = new GraphData();
data.xValues = AlphaValues;
data.AddData(ClValues2, GUIColors.GetColor(0) * 0.5f, "Cl2", false);
data.AddData(ClValues, GUIColors.GetColor(0), "Cl", true);
data.AddData(CdValues2, GUIColors.GetColor(1) * 0.5f, "Cd2", false);
data.AddData(CdValues, GUIColors.GetColor(1), "Cd", true);
data.AddData(CmValues2, GUIColors.GetColor(2) * 0.5f, "Cm2", false);
data.AddData(CmValues, GUIColors.GetColor(2), "Cm", true);
data.AddData(LDValues2, GUIColors.GetColor(3) * 0.5f, "L/D2", false);
data.AddData(LDValues, GUIColors.GetColor(3), "L/D", true);
return(data);
}
public GraphData AngleOfAttackSweep(
double machNumber,
double pitch,
double lowerBound,
double upperBound,
int numPoints,
int flapSetting,
bool spoilers,
CelestialBody body
)
{
if (machNumber.NearlyEqual(0))
{
machNumber = 0.001;
}
var input = new InstantConditionSimInput(0, 0, 0, 0, 0, 0, machNumber, pitch, flapSetting, spoilers);
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
var ClValues = new double[numPoints];
var CdValues = new double[numPoints];
var CmValues = new double[numPoints];
var LDValues = new double[numPoints];
var AlphaValues = new double[numPoints];
var ClValues2 = new double[numPoints];
var CdValues2 = new double[numPoints];
var CmValues2 = new double[numPoints];
var LDValues2 = new double[numPoints];
for (int i = 0; i < 2 * numPoints; i++)
{
double angle;
if (i < numPoints)
{
angle = i / (double)numPoints * (upperBound - lowerBound) + lowerBound;
}
else
{
angle = (i - (double)numPoints + 1) / numPoints * (lowerBound - upperBound) + upperBound;
}
input.alpha = angle;
_instantCondition.GetClCdCmSteady(input, out InstantConditionSimOutput output, i == 0);
if (i < numPoints)
{
AlphaValues[i] = angle;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
else
{
ClValues2[numPoints * 2 - 1 - i] = output.Cl;
CdValues2[numPoints * 2 - 1 - i] = output.Cd;
CmValues2[numPoints * 2 - 1 - i] = output.Cm;
LDValues2[numPoints * 2 - 1 - i] = output.Cl * 0.1 / output.Cd;
}
}
var data = new GraphData {
xValues = AlphaValues
};
data.AddData(ClValues2, FARConfig.GUIColors.ClColor * 0.5f, "Cl2", false);
data.AddData(ClValues, FARConfig.GUIColors.ClColor, Localizer.Format("FARAbbrevCl"), true);
data.AddData(CdValues2, FARConfig.GUIColors.CdColor * 0.5f, "Cd2", false);
data.AddData(CdValues, FARConfig.GUIColors.CdColor, Localizer.Format("FARAbbrevCd"), true);
data.AddData(CmValues2, FARConfig.GUIColors.CmColor * 0.5f, "Cm2", false);
data.AddData(CmValues, FARConfig.GUIColors.CmColor, Localizer.Format("FARAbbrevCm"), true);
data.AddData(LDValues2, FARConfig.GUIColors.LdColor * 0.5f, "L/D2", false);
data.AddData(LDValues, FARConfig.GUIColors.LdColor, Localizer.Format("FARAbbrevL_D"), true);
return(data);
}
public GraphData AngleOfAttackSweep(double machNumber, double pitch, double lowerBound, double upperBound, int numPoints, int flapSetting, bool spoilers, CelestialBody body)
{
if (machNumber < 1E-3)
{
machNumber = 1E-3;
}
FARAeroUtil.UpdateCurrentActiveBody(body);
FARAeroUtil.ResetEditorParts();
double[] ClValues = new double[(int)numPoints];
double[] CdValues = new double[(int)numPoints];
double[] CmValues = new double[(int)numPoints];
double[] LDValues = new double[(int)numPoints];
double[] AlphaValues = new double[(int)numPoints];
double[] ClValues2 = new double[(int)numPoints];
double[] CdValues2 = new double[(int)numPoints];
double[] CmValues2 = new double[(int)numPoints];
double[] LDValues2 = new double[(int)numPoints];
InstantConditionSimInput input = new InstantConditionSimInput(0, 0, 0, 0, 0, 0, FlightEnv.NewDefaultVal(body), pitch, flapSetting, spoilers);
input.fltenv.MachNumber = machNumber;
for (int i = 0; i < 2 * numPoints; i++)
{
double angle = 0;
if (i < numPoints)
{
angle = lowerBound + (upperBound - lowerBound) * (i == 0? 0 : i / (numPoints - 1.0));
}
else
{
angle = upperBound + (lowerBound - upperBound) * (i == numPoints ? 0 : (i - numPoints) / (numPoints - 1.0));
}
input.alpha = angle;
InstantConditionSimOutput output;
_instantCondition.GetClCdCmSteady(input, out output, i == 0, false);
if (i < numPoints)
{
AlphaValues[i] = angle;
ClValues[i] = output.Cl;
CdValues[i] = output.Cd;
CmValues[i] = output.Cm;
LDValues[i] = output.Cl * 0.1 / output.Cd;
}
else
{
ClValues2[numPoints * 2 - 1 - i] = output.Cl;
CdValues2[numPoints * 2 - 1 - i] = output.Cd;
CmValues2[numPoints * 2 - 1 - i] = output.Cm;
LDValues2[numPoints * 2 - 1 - i] = output.Cl * 0.1 / output.Cd;
}
}
GraphData data = new GraphData();
data.xValues = AlphaValues;
data.AddData(ClValues2, GUIColors.GetColor(0) * 0.5f, "Cl2", false);
data.AddData(ClValues, GUIColors.GetColor(0), Localizer.Format("FARAbbrevCl"), true);
data.AddData(CdValues2, GUIColors.GetColor(1) * 0.5f, "Cd2", false);
data.AddData(CdValues, GUIColors.GetColor(1), Localizer.Format("FARAbbrevCd"), true);
data.AddData(CmValues2, GUIColors.GetColor(2) * 0.5f, "Cm2", false);
data.AddData(CmValues, GUIColors.GetColor(2), Localizer.Format("FARAbbrevCm"), true);
data.AddData(LDValues2, GUIColors.GetColor(3) * 0.5f, "L/D2", false);
data.AddData(LDValues, GUIColors.GetColor(3), Localizer.Format("FARAbbrevL_D"), true);
data.exportdata.AddSizeVariables(_instantCondition, pitch, flapSetting, spoilers);
data.exportdata.AddAoASweepXVariable(machNumber, AlphaValues);
data.exportdata.AddYVariables(data);
return(data);
}
public void LateUpdate()
{
if (!CompatibilityChecker.IsAllCompatible())
{
return;
}
FARAeroUtil.ResetEditorParts();
FARBaseAerodynamics.GlobalCoLReady = false;
if (EditorLogic.fetch)
{
if (editorGUI == null)
{
editorGUI = new FAREditorGUI();
//editorGUI.LoadGUIParameters();
editorGUI.RestartCtrlGUI();
}
if (EditorLogic.startPod != null)
{
var editorShip = FARAeroUtil.AllEditorParts;
if (FARAeroUtil.EditorAboutToAttach() && count++ >= 10)
{
EditorPartsChanged = true;
count = 0;
}
if (part_count_all != editorShip.Count || part_count_ship != EditorLogic.SortedShipList.Count || EditorPartsChanged)
{
FindPartsWithoutFARModel(editorShip);
for (int i = 0; i < editorShip.Count; i++)
{
Part p = editorShip[i];
for (int j = 0; j < p.Modules.Count; j++)
{
PartModule m = p.Modules[j];
if (m is FARBaseAerodynamics)
{
(m as FARBaseAerodynamics).ClearShielding();
}
}
}
for (int i = 0; i < editorShip.Count; i++)
{
Part p = editorShip[i];
for (int j = 0; j < p.Modules.Count; j++)
{
PartModule m = p.Modules[j];
if (m is FARPartModule)
{
(m as FARPartModule).ForceOnVesselPartsChange();
}
}
}
part_count_all = editorShip.Count;
part_count_ship = EditorLogic.SortedShipList.Count;
EditorPartsChanged = false;
}
}
}
}