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 InstantConditionSimVars(InstantConditionSim parent, CelestialBody body, double altitude, double machNumber, double neededCl, double beta, double phi, int flap, bool spoilers)
{
this.parent = parent;
this.neededCl = neededCl;
this.CoM = parent.GetCoM();
FlightEnv fltenv = FlightEnv.NewSim(body, altitude, machNumber);
iterationInput = new InstantConditionSimInput(0, beta, phi, 0, 0, 0, fltenv, 0, flap, spoilers);
iterationOutput = new InstantConditionSimOutput();
}