#include "FGOutput.h"
#include "FGMatrix.h"
+static const char *IdSrc = "$Header$";
+static const char *IdHdr = ID_AUXILIARY;
+
/*******************************************************************************
************************************ CODE **************************************
*******************************************************************************/
Name = "FGAuxiliary";
vcas = veas = mach = qbar = pt = 0;
psl = rhosl = 1;
+ earthPosAngle = 0.0;
}
veas = sqrt(2*qbar/rhosl);
vPilotAccel = Translation->GetUVWdot() + Aircraft->GetXYZep() * Rotation->GetPQRdot();
-
-
+
+
+
+ earthPosAngle += State->Getdt()*OMEGA_EARTH;
} else {
}