}
}
- long_trim=0;
if(Aft_trim) long_trim = long_trim - trim_inc;
if(Fwd_trim) long_trim = long_trim + trim_inc;
/* printf("Long_control: %7.4f, long_trim: %7.4f,DEG_TO_RAD: %7.4f, RAD_TO_DEG: %7.4f\n",Long_control,long_trim,DEG_TO_RAD,RAD_TO_DEG);
*/ /*scale pct control to degrees deflection*/
- if ((Long_control+long_trim) <= 0)
- elevator=(Long_control+long_trim)*28*DEG_TO_RAD;
+ if ((Long_control+Long_trim) <= 0)
+ elevator=(Long_control+Long_trim)*28*DEG_TO_RAD;
else
- elevator=(Long_control+long_trim)*23*DEG_TO_RAD;
+ elevator=(Long_control+Long_trim)*23*DEG_TO_RAD;
aileron = -1*Lat_control*17.5*DEG_TO_RAD;
rudder = -1*Rudder_pedal*16*DEG_TO_RAD;