用记事本打开文件,找到一下。
-- thrust values IGNORE
thrustNormalMin = 70 -- minimum thrust power (at the end of the speed interval) IGNORE
thrustNormalMax = 100 -- maximum thrust power (at the start of the speed interval) IGNORE
thrustAfterburnerMin = 100 -- minimum afterburner power IGNORE
thrustAfterburnerMax = 140 -- maximum afterburner power IGNORE
把上述的四个参数(飞机加速)尽量往大改,我是给后面都加了两个零。
function ThrustFormula (currentThrustValue,thrustPercentage,thrusterScale,planeVelocity,planeMass,fricForce)
local thrustForce = 0
gplaneVelocity = planeVelocity
if (gplaneVelocity < 1200) then
thrustForce = (thrustPercentage - 50) * 0.02 * currentThrustValue * planeMass
else
if (gplaneVelocity) then
local thrustDiv = Lerp (0,1,(gplaneVelocity/maxVelocity_used))
-- print (gplaneVelocity,maxVelocity_used,thrustDiv)
if (thrustDiv <= 0.2) then
thrustDiv = 0.2
end
if (thrustDiv > 1) then
thrustDiv=1
end