plane: adjusted parameters

This commit is contained in:
Erkki Seppälä 2014-10-20 20:50:31 +03:00
parent 9765ae8daa
commit bc968b2b4c

View file

@ -56,9 +56,9 @@ local lift = function(angle)
return 1.68429 * math.exp(-math.pow(angle / math.pi * 180.0 -17.3801, 2.0) / (2.0 * math.pow(15.0, 2.0)))
end
local fwd_frict_coeff = 0.5
local nor_frict_coeff = 0.9
local tail_frict_coeff = 0.5
local fwd_frict_coeff = 0.1
local nor_frict_coeff = 0.8
local tail_frict_coeff = 0.4
local tail_area = 5.0
local turn_coeff = 500.0
local wing_lift = 0.5
@ -67,7 +67,7 @@ local decel_speed = 400.0
local max_motorPower = ENGINE_MAX
local head_area = 1.0
local plane_area = 10.0
local motor_speed_ratio = 100.0
local motor_speed_ratio = 80.0
local out_of_bounds_coeff_multiplier = 10.0