Sync. w. JSB CVS as of 15/01/2007

[flightgear.git] / src / FDM / LaRCsim / cherokee_aero.c

diff --git a/src/FDM/LaRCsim/cherokee_aero.c b/src/FDM/LaRCsim/cherokee_aero.c
index e74f2e5dc1f01eba28bb8cdcd4cecc30cc9a8b4f..46f738ae85c507f4d2345f03ada7342e5e591270 100644 (file)
--- a/src/FDM/LaRCsim/cherokee_aero.c
+++ b/src/FDM/LaRCsim/cherokee_aero.c
@@ -138,14 +138,14 @@ void cherokee_aero()
 
 
 
-               Cz = Cz0 + Cza*Alpha + Czat*(Alpha_dot*c/2.0/V) + Czq*(q*c/2.0/V) + Czde * elevator;
-               Cm = Cm0 + Cma*Alpha + Cmat*(Alpha_dot*c/2.0/V) + Cmq*(q*c/2.0/V) + Cmde * elevator; 
+               Cz = Cz0 + Cza*Std_Alpha + Czat*(Std_Alpha_dot*c/2.0/V) + Czq*(q*c/2.0/V) + Czde * elevator;
+               Cm = Cm0 + Cma*Std_Alpha + Cmat*(Std_Alpha_dot*c/2.0/V) + Cmq*(q*c/2.0/V) + Cmde * elevator; 
 
-               Cx = Cx0 - (Cza*Alpha)*(Cza*Alpha)/(LS_PI*5.71*0.6);
-               Cl = Clb*Beta + Clp*(p*b/2.0/V) + Clr*(r*b/2.0/V) + Clda * aileron;
+               Cx = Cx0 - (Cza*Std_Alpha)*(Cza*Std_Alpha)/(LS_PI*5.71*0.6);
+               Cl = Clb*Std_Beta + Clp*(p*b/2.0/V) + Clr*(r*b/2.0/V) + Clda * aileron;
 
-               Cy = Cyb*Beta + Cyr*(r*b/2.0/V); 
-               Cn = Cnb*Beta + Cnp*(p*b/2.0/V) + Cnr*(r*b/2.0/V) + Cndr * rudder; 
+               Cy = Cyb*Std_Beta + Cyr*(r*b/2.0/V); 
+               Cn = Cnb*Std_Beta + Cnp*(p*b/2.0/V) + Cnr*(r*b/2.0/V) + Cndr * rudder; 
 
 /* back to body axes */
        {