fdm->v_north = 0.0;
fdm->v_east = 0.0;
fdm->v_down = 0.0;
- fdm->v_wind_body_north = 0.0;
- fdm->v_wind_body_east = 0.0;
- fdm->v_wind_body_down = 0.0;
+ fdm->v_body_u = 0.0;
+ fdm->v_body_v = 0.0;
+ fdm->v_body_w = 0.0;
fdm->stall_warning = 0.0;
fdm->A_X_pilot = 0.0;
htonf(fdm->v_north);
htonf(fdm->v_east);
htonf(fdm->v_down);
- htonf(fdm->v_wind_body_north);
- htonf(fdm->v_wind_body_east);
- htonf(fdm->v_wind_body_down);
+ htonf(fdm->v_body_u);
+ htonf(fdm->v_body_v);
+ htonf(fdm->v_body_w);
htonf(fdm->A_X_pilot);
htonf(fdm->A_Y_pilot);