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fixed error in pitch correction when using conventional landing gear

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This commit is contained in:
Alexsandro Percy 2023-07-17 13:15:14 -03:00
parent fd728c2dff
commit dd58627099
1 changed files with 2 additions and 2 deletions
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4
lib_planes/entities.lua
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@ -296,7 +296,7 @@ function airutils.logic(self)
newpitch = math.rad(self._angle_of_attack) newpitch = math.rad(self._angle_of_attack)
else else
--ajustar angulo de ataque --ajustar angulo de ataque
if longit_speed > (self._min_speed) then if longit_speed > self._min_speed then
local percentage = math.abs(((longit_speed * 100)/(self._min_speed + 5))/100) local percentage = math.abs(((longit_speed * 100)/(self._min_speed + 5))/100)
if percentage > 1.5 then percentage = 1.5 end if percentage > 1.5 then percentage = 1.5 end
self._angle_of_attack = self._wing_angle_of_attack - ((self._elevator_angle / self._elevator_response_attenuation)*percentage) self._angle_of_attack = self._wing_angle_of_attack - ((self._elevator_angle / self._elevator_response_attenuation)*percentage)
@ -321,7 +321,7 @@ function airutils.logic(self)
--minetest.chat_send_all(self._angle_of_attack) --minetest.chat_send_all(self._angle_of_attack)
-- adjust pitch at ground -- adjust pitch at ground
if math.abs(longit_speed) > self._tail_lift_min_speed then if math.abs(longit_speed) > self._tail_lift_min_speed and is_flying == false then
newpitch = ground_pitch(self, longit_speed, newpitch) newpitch = ground_pitch(self, longit_speed, newpitch)
else else
if math.abs(longit_speed) < self._tail_lift_min_speed then if math.abs(longit_speed) < self._tail_lift_min_speed then