berengma/airutils
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

added more control do lift

Browse Source
This commit is contained in:
Alexsandro Percy 2023-07-07 20:36:18 -03:00
parent 4f26cbd07d
commit 92746d795e
1 changed files with 8 additions and 15 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

23
init.lua
View File

@ -250,20 +250,6 @@ function airutils.getLiftAccel(self, velocity, accel, longit_speed, roll, curr_p
local vel_wind = vector.multiply(accel_wind, self.dtime)
local new_velocity = vector.add(velocity, vel_wind)
--[[local hull_direction = airutils.rot_to_dir(self.object:get_rotation())
local wind_yaw = minetest.dir_to_yaw(wind)
local orig_vel = vector.dot(velocity,hull_direction)
local new_vel = vector.dot(vel_wind,hull_direction)
if orig_vel > new_vel then
orig_vel = core.colorize('#00ff00', orig_vel)
new_vel = core.colorize('#ff0000', new_vel)
else
orig_vel = core.colorize('#ff0000', orig_vel)
new_vel = core.colorize('#00ff00', new_vel)
end
minetest.chat_send_all("velocity: "..orig_vel.." - new: "..new_vel.." - dir: "..math.deg(wind_yaw) )]]--
velocity = new_velocity
if longit_speed == nil then longit_speed = 0 end
wingspan = wingspan or 10
local ground_effect_extra_lift = airutils.get_ground_effect_lift(self, curr_pos, lift, wingspan)
@ -279,7 +265,14 @@ function airutils.getLiftAccel(self, velocity, accel, longit_speed, roll, curr_p
local retval = accel
local min_speed = 1;
if self._min_speed then min_speed = self._min_speed end
min_speed = min_speed / 2
if longit_speed > min_speed then
local striped_velocity = {x=velocity.x, y=velocity.y, z=velocity.z}
local cut_velocity = (min_speed * 1)/longit_speed
striped_velocity.x = striped_velocity.x - (striped_velocity.x * cut_velocity)
striped_velocity.z = striped_velocity.z - (striped_velocity.z * cut_velocity)
local angle_of_attack = math.rad(self._angle_of_attack + wing_config)
--local acc = 0.8
local daoa = deg(angle_of_attack)
@ -299,7 +292,7 @@ function airutils.getLiftAccel(self, velocity, accel, longit_speed, roll, curr_p
local lift_dir = vector.normalize(vector.cross(cross,hdir))
local lift_coefficient = (0.24*abs(daoa)*(1/(0.025*daoa+3))^4*math.sign(daoa))
local lift_val = math.abs((lift*(vector.length(velocity)^2)*lift_coefficient)*curr_percent_height)
local lift_val = math.abs((lift*(vector.length(striped_velocity)^2)*lift_coefficient)*curr_percent_height)
if lift_val < 1 then lift_val = 1 end -- hipotetical aerodinamic wing will have no "lift" for down
--minetest.chat_send_all('lift: '.. lift_val)