#include "ls_types.h"
#include "ls_generic.h"
#include "ls_cockpit.h"
+#include "ls_constants.h"
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;
- Cx = Cx0 - (Cza*Alpha)*(Cza*Alpha)/(M_PI*5.71*0.6);
+ 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;
Cy = Cyb*Beta + Cyr*(r*b/2.0/V);