plane: adjusted parameters
This commit is contained in:
parent
9765ae8daa
commit
bc968b2b4c
1 changed files with 4 additions and 4 deletions
|
@ -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)))
|
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
|
end
|
||||||
|
|
||||||
local fwd_frict_coeff = 0.5
|
local fwd_frict_coeff = 0.1
|
||||||
local nor_frict_coeff = 0.9
|
local nor_frict_coeff = 0.8
|
||||||
local tail_frict_coeff = 0.5
|
local tail_frict_coeff = 0.4
|
||||||
local tail_area = 5.0
|
local tail_area = 5.0
|
||||||
local turn_coeff = 500.0
|
local turn_coeff = 500.0
|
||||||
local wing_lift = 0.5
|
local wing_lift = 0.5
|
||||||
|
@ -67,7 +67,7 @@ local decel_speed = 400.0
|
||||||
local max_motorPower = ENGINE_MAX
|
local max_motorPower = ENGINE_MAX
|
||||||
local head_area = 1.0
|
local head_area = 1.0
|
||||||
local plane_area = 10.0
|
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
|
local out_of_bounds_coeff_multiplier = 10.0
|
||||||
|
|
||||||
|
|
Loading…
Reference in a new issue