private void setupPullup()
{
#if TODO
double g, q, cgamma;
g = fdmex.Inertial.Gravity;
cgamma = Math.Cos(fgic.GetFlightPathAngleRadIC());
if (log.IsDebugEnabled)
{
log.Debug("setPitchRateInPullup(): " + g + ", " + cgamma + ", "
+ fgic.VtrueFpsIC);
}
q = g * (targetNlf - cgamma) / fgic.VtrueFpsIC;
if (log.IsDebugEnabled)
{
log.Debug(targetNlf + ", " + q);
}
fgic.QRadpsIC = q;
if (log.IsDebugEnabled)
{
log.Debug("setPitchRateInPullup() complete");
}
#endif
throw new NotImplementedException("Pending upgrade to lastest version of JSBSIM");
}
public void TestDefaultConstructor()
{
FDMExecutive fdmex = new FDMExecutive();
InitialCondition ic = new InitialCondition(fdmex);
Assert.AreEqual(0.0, ic.GetLatitudeDegIC());
Assert.AreEqual(0.0, ic.GetLatitudeRadIC());
Assert.AreEqual(0.0, ic.GetLongitudeDegIC());
Assert.AreEqual(0.0, ic.GetLongitudeRadIC());
Assert.AreEqual(0.0, ic.GetGeodLatitudeDegIC());
Assert.AreEqual(0.0, ic.GetGeodLatitudeRadIC());
Assert.AreEqual(0.0, ic.GetThetaDegIC());
Assert.AreEqual(0.0, ic.GetThetaRadIC());
Assert.AreEqual(0.0, ic.GetPhiDegIC());
Assert.AreEqual(0.0, ic.GetPhiRadIC());
Assert.AreEqual(0.0, ic.GetPsiDegIC());
Assert.AreEqual(0.0, ic.GetPsiRadIC());
Assert.AreEqual(0.0, ic.GetAltitudeASLFtIC());
Assert.AreEqual(0.0, ic.GetAltitudeAGLFtIC());
Assert.AreEqual(0.0, ic.GetEarthPositionAngleIC());
Assert.AreEqual(0.0, ic.GetTerrainElevationFtIC());
Assert.AreEqual(0.0, ic.GetVcalibratedKtsIC());
Assert.AreEqual(0.0, ic.GetVequivalentKtsIC());
Assert.AreEqual(0.0, ic.GetVgroundFpsIC());
Assert.AreEqual(0.0, ic.GetVtrueFpsIC());
Assert.AreEqual(0.0, ic.GetMachIC());
Assert.AreEqual(0.0, ic.GetClimbRateFpsIC());
Assert.AreEqual(0.0, ic.GetFlightPathAngleDegIC());
Assert.AreEqual(0.0, ic.GetFlightPathAngleRadIC());
Assert.AreEqual(0.0, ic.GetAlphaDegIC());
Assert.AreEqual(0.0, ic.GetAlphaRadIC());
Assert.AreEqual(0.0, ic.GetBetaDegIC());
Assert.AreEqual(0.0, ic.GetBetaDegIC());
Assert.AreEqual(0.0, ic.GetBetaRadIC());
Assert.AreEqual(0.0, ic.GetWindFpsIC());
Assert.AreEqual(0.0, ic.GetWindDirDegIC());
Assert.AreEqual(0.0, ic.GetWindUFpsIC());
Assert.AreEqual(0.0, ic.GetWindVFpsIC());
Assert.AreEqual(0.0, ic.GetWindWFpsIC());
Assert.AreEqual(0.0, ic.GetWindNFpsIC());
Assert.AreEqual(0.0, ic.GetWindEFpsIC());
Assert.AreEqual(0.0, ic.GetWindDFpsIC());
Assert.AreEqual(0.0, ic.GetUBodyFpsIC());
Assert.AreEqual(0.0, ic.GetVBodyFpsIC());
Assert.AreEqual(0.0, ic.GetWBodyFpsIC());
Assert.AreEqual(0.0, ic.GetVNorthFpsIC());
Assert.AreEqual(0.0, ic.GetVEastFpsIC());
Assert.AreEqual(0.0, ic.GetVDownFpsIC());
Assert.AreEqual(0.0, ic.GetPRadpsIC());
Assert.AreEqual(0.0, ic.GetQRadpsIC());
Assert.AreEqual(0.0, ic.GetRRadpsIC());
// TS_ASSERT_VECTOR_EQUALS(ic.GetWindNEDFpsIC(), zero);
//TS_ASSERT_VECTOR_EQUALS(ic.GetUVWFpsIC(), zero);
//TS_ASSERT_VECTOR_EQUALS(ic.GetPQRRadpsIC(), zero);
}
private void setupPullup()
{
double g, q, cgamma;
g = fdmex.Inertial.Gravity;
cgamma = Math.Cos(fgic.GetFlightPathAngleRadIC());
if (log.IsDebugEnabled)
{
log.Debug("setPitchRateInPullup(): " + g + ", " + cgamma + ", "
+ fgic.VtrueFpsIC);
}
q = g * (targetNlf - cgamma) / fgic.VtrueFpsIC;
if (log.IsDebugEnabled)
{
log.Debug(targetNlf + ", " + q);
}
fgic.QRadpsIC = q;
if (log.IsDebugEnabled)
{
log.Debug("setPitchRateInPullup() complete");
}
}