Improve timing statistics

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

diff --git a/src/FDM/LaRCsim/navion_aero.c b/src/FDM/LaRCsim/navion_aero.c
index 6839e457c37de4371875bd3bd9c878522ce34a91..b56bc08af4fc58061f165374e17d3284bd4e84c0 100644 (file)
--- a/src/FDM/LaRCsim/navion_aero.c
+++ b/src/FDM/LaRCsim/navion_aero.c
@@ -112,7 +112,7 @@ ring is given below:
 extern COCKPIT cockpit_;
 
 
-void aero( SCALAR dt, int Initialize ) {
+void navion_aero( SCALAR dt, int Initialize ) {
   static int init = 0;
 
   SCALAR u, w;
@@ -202,10 +202,10 @@ void aero( SCALAR dt, int Initialize ) {
   F_Y_aero = scale*(Mass*Y_v*V_body);
   F_Z_aero = scale*(Z_0 + Mass*(Z_u*u + Z_w*w + Z_de*elevator));
   
-  M_l_aero = scale*(I_xx*(L_beta*Beta + L_p*P_body + L_r*R_body
+  M_l_aero = scale*(I_xx*(L_beta*Std_Beta + L_p*P_body + L_r*R_body
                   + L_da*aileron + L_dr*rudder));
   M_m_aero = scale*(M_0 + I_yy*(M_w*w + M_q*Q_body + M_de*(elevator + Long_trim)));
-  M_n_aero = scale*(I_zz*(N_beta*Beta + N_p*P_body + N_r*R_body
+  M_n_aero = scale*(I_zz*(N_beta*Std_Beta + N_p*P_body + N_r*R_body
                   + N_da*aileron + N_dr*rudder));
   
 }