From 952474baf44b2dfe5d65cb1c2ecd51d582e4e975 Mon Sep 17 00:00:00 2001 From: fwongkwok <53922077+fwongkwok@users.noreply.github.com> Date: Sun, 6 Sep 2020 15:47:54 +1000 Subject: [PATCH] fixed aero gain issue --- mur_2019/data/aero.ini | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/mur_2019/data/aero.ini b/mur_2019/data/aero.ini index e979e5e..9ee838d 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) -- GitLab