$Header$
$Log$
+Revision 1.4 2003/05/25 12:14:46 ehofman
+Rename some defines to prevent a namespace clash
+
Revision 1.3 2003/05/13 18:45:06 curt
Robert Deters:
if( (v_XZ_plane_2 == 0) || (V_rel_wind == 0) )
{
- Alpha_dot = 0;
- Beta_dot = 0;
+ Std_Alpha_dot = 0;
+ Std_Beta_dot = 0;
}
else
{
- Alpha_dot = (U_body*W_dot_body - W_body*U_dot_body)/
+ Std_Alpha_dot = (U_body*W_dot_body - W_body*U_dot_body)/
v_XZ_plane_2;
- Beta_dot = (signU*v_XZ_plane_2*V_dot_body
+ Std_Beta_dot = (signU*v_XZ_plane_2*V_dot_body
- V_body*(U_body*U_dot_body + W_body*W_dot_body))
/(V_rel_wind*V_rel_wind*sqrt(v_XZ_plane_2));
}
/* Calculate flight path and other flight condition values */
if (U_body == 0)
- Alpha = 0;
+ Std_Alpha = 0;
else
- Alpha = atan2( W_body, U_body );
+ Std_Alpha = atan2( W_body, U_body );
- Cos_alpha = cos(Alpha);
- Sin_alpha = sin(Alpha);
+ Cos_alpha = cos(Std_Alpha);
+ Sin_alpha = sin(Std_Alpha);
if (V_rel_wind == 0)
- Beta = 0;
+ Std_Beta = 0;
else
- Beta = asin( V_body/ V_rel_wind );
+ Std_Beta = asin( V_body/ V_rel_wind );
- Cos_beta = cos(Beta);
- Sin_beta = sin(Beta);
+ Cos_beta = cos(Std_Beta);
+ Sin_beta = sin(Std_Beta);
V_true_kts = V_rel_wind * V_TO_KNOTS;