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added option for cannard and pendulum planes

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This commit is contained in:
Alexsandro Percy 2023-09-03 19:49:20 -03:00
parent 19acdce0fa
commit be966a1ed8
1 changed files with 11 additions and 3 deletions
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14
lib_planes/entities.lua
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@ -313,12 +313,17 @@ function airutils.logic(self)
newpitch = airutils.get_plane_pitch(velocity, longit_speed, self._min_speed, self._angle_of_attack)
end
--for airplanes with cannard or pendulum wing
local actuator_angle = self._elevator_angle
if self._inverted_pitch_reaction then actuator_angle = -1*self._elevator_angle end
--is an stall, force a recover
if longit_speed < (self._min_speed+0.5) and climb_rate < -1.5 and is_flying then
if player and self.driver_name then
--minetest.chat_send_player(self.driver_name,core.colorize('#ff0000', " >>> STALL"))
end
self._elevator_angle = 0
actuator_angle = 0
self._angle_of_attack = -1
newpitch = math.rad(self._angle_of_attack)
else
@ -326,7 +331,7 @@ function airutils.logic(self)
if longit_speed > self._min_speed then
local percentage = math.abs(((longit_speed * 100)/(self._min_speed + 5))/100)
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 - ((actuator_angle / self._elevator_response_attenuation)*percentage)
--set the plane on level
if airutils.adjust_attack_angle_by_speed then
@ -336,12 +341,15 @@ function airutils.logic(self)
if self._angle_of_attack < self._min_attack_angle then
self._angle_of_attack = self._min_attack_angle
self._elevator_angle = self._elevator_angle - 0.2
actuator_angle = actuator_angle - 0.2
end --limiting the negative angle]]--
--[[if self._angle_of_attack > self._max_attack_angle then
self._angle_of_attack = self._max_attack_angle
self._elevator_angle = self._elevator_angle + 0.2
actuator_angle = actuator_angle + 0.2
end --limiting the very high climb angle due to strange behavior]]--]]--
if self._inverted_pitch_reaction then self._elevator_angle = -1*actuator_angle end --revert the reversion
end
end