diff --git a/mur_2019/data/aero.ini b/mur_2019/data/aero.ini
index e979e5e373c8dfe3aded147845434b41e7694eaf..9ee838d8fde8b36f2dafc578c977feb6ce5fd1a3 100644
--- a/mur_2019/data/aero.ini
+++ b/mur_2019/data/aero.ini
@@ -9,10 +9,10 @@ SPAN=1.0								; width of the wing in meters. both help determine the frontal a
 POSITION=0,0.278,0						; position in x,y,z starting from the CoG
 LUT_AOA_CL=wing_body_AOA_CL.lut			; Coefficient of Lift lookup table
 LUT_GH_CL=								; Height aero lift multiplier lookup table
-CL_GAIN=6.0								; Coefficient of Lift multiplier (for easy fine tuning) 
+CL_GAIN=1								; Coefficient of Lift multiplier (for easy fine tuning) 
 LUT_AOA_CD=wing_body_AOA_CD.lut			; Coefficient of drag lookup table
 LUT_GH_CD=								; Height aero drag multiplier table
-CD_GAIN=6.0								; Coefficient of drag multiplier (for easy fine tuning)
+CD_GAIN=1								; Coefficient of drag multiplier (for easy fine tuning)
 ANGLE=0									; Default starting wing angle (degrees)
 ZONE_FRONT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
 ZONE_FRONT_CD=0    ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)