diff --git a/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c b/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c index b868d790b6..571cb43048 100644 --- a/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c +++ b/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c @@ -208,7 +208,7 @@ void h_ctl_course_loop ( void ) { */ // Heading error - float herr = *stateGetNedToBodyEulers_f()->psi - h_ctl_course_setpoint; //+crab); + float herr = stateGetNedToBodyEulers_f()->psi - h_ctl_course_setpoint; //+crab); NormRadAngle(herr); if (advance < -0.5) // 90 degree turn