diff --git a/src/main/flight/pid.c b/src/main/flight/pid.c
index a21ae688d3..0623c826b6 100644
--- a/src/main/flight/pid.c
+++ b/src/main/flight/pid.c
@@ -871,7 +871,7 @@ static void NOINLINE pidTurnAssistant(pidState_t *pidState)
             airspeedForCoordinatedTurn = constrainf(airspeedForCoordinatedTurn, 300, 6000);
 
             // Calculate rate of turn in Earth frame according to FAA's Pilot's Handbook of Aeronautical Knowledge
-            float bankAngleTarget = pidRcCommandToAngle(rcCommand[FD_ROLL], pidProfile()->max_angle_inclination[FD_ROLL]);
+            float bankAngleTarget = DECIDEGREES_TO_RADIANS(pidRcCommandToAngle(rcCommand[FD_ROLL], pidProfile()->max_angle_inclination[FD_ROLL]));
             float coordinatedTurnRateEarthFrame = GRAVITY_CMSS * tan_approx(-bankAngleTarget) / airspeedForCoordinatedTurn;
 
             targetRates.z = RADIANS_TO_DEGREES(coordinatedTurnRateEarthFrame);