#include "FGAircraft.h"
#include "FGPosition.h"
#include "FGOutput.h"
+#include "FGMatrix.h"
/*******************************************************************************
************************************ CODE **************************************
Name = "FGAuxiliary";
vcas = veas = mach = qbar = pt = 0;
psl = rhosl = 1;
+ earthPosAngle = 0.0;
}
A = pow(((pt-p)/psl+1),0.28571);
vcas = sqrt(7*psl/rhosl*(A-1));
veas = sqrt(2*qbar/rhosl);
-
-
+
+ vPilotAccel = Translation->GetUVWdot() + Aircraft->GetXYZep() * Rotation->GetPQRdot();
+
+
+
+ earthPosAngle += State->Getdt()*OMEGA_EARTH;
} else {
}