//------------------------------------------------------------------------------
// virtual void LoadData()
//------------------------------------------------------------------------------
void ThrusterCoefficientDialog::LoadData()
{
Integer paramID = 0;
int coefCount = Thruster::COEFFICIENT_COUNT;
std::stringstream cStrings("");
std::stringstream kStrings("");
if (coefType == "C")
{
std::stringstream cStrings("");
for (Integer ii = 0; ii < coefCount; ii++)
{
cStrings << "C" << ii + 1;
coefNames.push_back(cStrings.str());
cStrings.str("");
}
paramID = theObject->GetParameterID("C_UNITS");
StringArray coefUnits = theObject->GetStringArrayParameter(paramID);
for (Integer i = 0; i < coefCount; i++)
{
coefGrid->SetCellValue(i, 0, coefNames[i].c_str());
coefGrid->SetCellValue(i, 1, wxVariant(coefValues[i]));
coefGrid->SetCellValue(i, 2, coefUnits[i].c_str());
}
}
else if (coefType == "K")
{
std::stringstream kStrings("");
for (Integer ii = 0; ii < coefCount; ii++)
{
kStrings << "K" << ii + 1;
coefNames.push_back(kStrings.str());
kStrings.str("");
}
paramID = theObject->GetParameterID("K_UNITS");
StringArray coefUnits = theObject->GetStringArrayParameter(paramID);
for (Integer i = 0; i < coefCount; i++)
{
coefGrid->SetCellValue(i, 0, coefNames[i].c_str());
coefGrid->SetCellValue(i, 1, wxVariant(coefValues[i]));
coefGrid->SetCellValue(i, 2, coefUnits[i].c_str());
}
}
}
//------------------------------------------------------------------------------
// void LoadData()
//------------------------------------------------------------------------------
void BurnThrusterPanel::LoadData()
{
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("BurnThrusterPanel::LoadData() entered\n");
#endif
// Set object pointer for "Show Script"
mObject = theObject;
bool isImpBurn = false;
if (theObject->GetType() == Gmat::IMPULSIVE_BURN)
isImpBurn = true;
if (isImpBurn)
{
thrustDir1 = "Element1";
thrustDir2 = "Element2";
thrustDir3 = "Element3";
}
else
{
thrustDir1 = "ThrustDirection1";
thrustDir2 = "ThrustDirection2";
thrustDir3 = "ThrustDirection3";
}
Integer paramID;
try
{
paramID = theObject->GetParameterID("CoordinateSystem");
coordSysName = theObject->GetStringParameter(paramID);
coordSysComboBox->SetValue(coordSysName.c_str());
paramID = theObject->GetParameterID("Origin");
std::string objName = theObject->GetStringParameter(paramID);
originComboBox->SetValue(objName.c_str());
paramID = theObject->GetParameterID("Axes");
objName = theObject->GetStringParameter(paramID);
axesComboBox->SetValue(objName.c_str());
paramID = theObject->GetParameterID(thrustDir1);
elem1TextCtrl->SetValue(wxVariant(theObject->GetRealParameter(paramID)));
paramID = theObject->GetParameterID(thrustDir2);
elem2TextCtrl->SetValue(wxVariant(theObject->GetRealParameter(paramID)));
paramID = theObject->GetParameterID(thrustDir3);
elem3TextCtrl->SetValue(wxVariant(theObject->GetRealParameter(paramID)));
paramID = theObject->GetParameterID("DecrementMass");
decMassCheckBox->SetValue((wxVariant(theObject->GetBooleanParameter(paramID))));
paramID = theObject->GetParameterID("GravitationalAccel");
gravityAccelTextCtrl->SetValue((wxVariant(theObject->GetRealParameter(paramID))));
paramID = theObject->GetParameterID("Tank");
StringArray tanks = theObject->GetStringArrayParameter(paramID);
if (tanks.empty())
{
if (theGuiManager->GetNumFuelTank() > 0)
{
tankComboBox->Insert("No Fuel Tank Selected", 0);
tankComboBox->SetSelection(0);
}
}
else
{
tankName = tanks[0];
tankComboBox->SetValue(STD_TO_WX_STRING(tankName.c_str()));
isTankEmpty = false;
}
// Disable tank combo box if decrement mass is not checked
if (!decMassCheckBox->IsChecked())
{
// Tanks needed to apply nontrivial coefficients, so don't disable
//tankLabel->Disable();
//tankComboBox->Disable();
// g is only used to decrement mass
gravityAccelLabel->Disable();
gravityAccelTextCtrl->Disable();
gravityAccelUnit->Disable();
if (theObject->GetType() == Gmat::IMPULSIVE_BURN)
{
ispLabel->Disable();
ispTextCtrl->Disable();
ispUnit->Disable();
}
}
else
{
// g is required to decrement mass
gravityAccelLabel->Enable();
gravityAccelTextCtrl->Enable();
gravityAccelUnit->Enable();
}
if (theObject->IsOfType(Gmat::THRUSTER))
{
if (theObject->IsOfType("ChemicalThruster"))
{
// Get the initial values for the coefficients
Integer cParamID = 0;
Integer kParamID = 0;
Integer coefCount = ChemicalThruster::COEFFICIENT_COUNT;
std::stringstream cStrings("");
std::stringstream kStrings("");
Real cVal, kVal;
for (Integer ii = 0; ii < coefCount; ii++)
{
cStrings << "C" << ii + 1;
cParamID = theObject->GetParameterID(cStrings.str());
cVal = theObject->GetRealParameter(cParamID);
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("Loading: %s = %lf\n", cStrings.str().c_str(), cVal);
#endif
cCoefs.push_back(cVal);
cCoefNames.push_back(cStrings.str());
cStrings.str("");
}
for (Integer ii = 0; ii < coefCount; ii++)
{
kStrings << "K" << ii + 1;
kParamID = theObject->GetParameterID(kStrings.str());
kVal = theObject->GetRealParameter(kParamID);
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("Loading: %s = %lf\n", kStrings.str().c_str(), kVal);
#endif
kCoefs.push_back(kVal);
kCoefNames.push_back(kStrings.str());
kStrings.str("");
}
}
else // Electric Thruster
{
// Get the initial values for the coefficients
Integer tParamID = 0;
Integer mfParamID = 0;
Integer coefCount = ElectricThruster::ELECTRIC_COEFF_COUNT;
std::stringstream tStrings("");
std::stringstream mfStrings("");
Real tVal, mfVal;
for (Integer ii = 0; ii < coefCount; ii++)
{
tStrings << "ThrustCoeff" << ii + 1;
tParamID = theObject->GetParameterID(tStrings.str());
tVal = theObject->GetRealParameter(tParamID);
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("Loading: %s = %lf\n", tStrings.str().c_str(), tVal);
#endif
tCoefs.push_back(tVal);
tCoefNames.push_back(tStrings.str());
tStrings.str("");
}
for (Integer ii = 0; ii < coefCount; ii++)
{
mfStrings << "MassFlowCoeff" << ii + 1;
mfParamID = theObject->GetParameterID(mfStrings.str());
mfVal = theObject->GetRealParameter(mfParamID);
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("Loading: %s = %lf\n", mfStrings.str().c_str(), mfVal);
#endif
mfCoefs.push_back(mfVal);
mfCoefNames.push_back(mfStrings.str());
mfStrings.str("");
}
}
}
// Update Origin and Axes
UpdateOriginAxes();
}
catch (BaseException &e)
{
MessageInterface::PopupMessage(Gmat::ERROR_, e.GetFullMessage());
}
#ifdef DEBUG_BURNPANEL_LOAD
MessageInterface::ShowMessage("BurnThrusterPanel::LoadData() exiting\n");
#endif
}