void valueInitialize()
{
_Acceleration = 0;
oldXRotation = transform.rotation.eulerAngles.x;
oldYRotation = transform.rotation.eulerAngles.y;
oldZRotation = transform.rotation.eulerAngles.z;
_gravity = _constval.GetGravity();
propellerDiameter = _constval.GetPropellerDiameter();
propellerVelocity = _constval.GetAngularVelocity();
maxRPM = _constval.GetMaxRPM();
airDensity = _constval.GetAirDensity();
thrustCoefficient = _constval.GetC_T();
powerCoefficient = _constval.GetC_Pow();
linearDragCoefficient = _constval.GetClin();
AngularDragCoefficient = _constval.GetC_AngularDrag();
}
void PropellerForce()
{
if ((Mathf.Abs(Input.GetAxis("Vertical")) > 0.2f) || (Mathf.Abs(Input.GetAxis("Horizontal")) > 0.2f))
{
if (Input.GetAxis("FlyUp") == 0 && (Mathf.Abs(Input.GetAxis("Vertical")) > 0.2f))
{
upForce = _constval.GetC_T() * _constval.GetAirDensity() * Mathf.Pow(_constval.GetAngularVelocity(), 2)
* Mathf.Pow(_constval.GetPropellerDiameter(), 4) * Mathf.Abs(Input.GetAxis("Vertical"));
curRPM = Mathf.Abs(_constval.GetMaxRPM() * Input.GetAxis("Vertical"));
tiltAmount = 40;
}
if (Input.GetAxis("FlyUp") == 0 && (Mathf.Abs(Input.GetAxis("Horizontal")) > 0.2f))
{
upForce = _constval.GetC_T() * _constval.GetAirDensity() * Mathf.Pow(_constval.GetAngularVelocity(), 2)
* Mathf.Pow(_constval.GetPropellerDiameter(), 4) * Mathf.Abs(Input.GetAxis("Horizontal"));
curRPM = Mathf.Abs(_constval.GetMaxRPM() * Input.GetAxis("Horizontal"));
tiltAmount = 40;
}
}
if (Mathf.Abs(Input.GetAxis("FlyUp")) >= 0.3f)
{
upForce = _constval.GetC_T() * _constval.GetAirDensity() * Mathf.Pow(_constval.GetAngularVelocity(), 2)
* Mathf.Pow(_constval.GetPropellerDiameter(), 4) * Input.GetAxis("FlyUp");
if ((Mathf.Abs(Input.GetAxis("Vertical")) != 0) || (Mathf.Abs(Input.GetAxis("Horizontal")) != 0))
{
tiltAmount = 20;
}
else
{
tiltAmount = 0;
}
curRPM = Mathf.Abs(_constval.GetMaxRPM() * Input.GetAxis("FlyUp"));
}
if (Input.GetAxis("FlyUp") == 0 && Input.GetAxis("Vertical") == 0 && Input.GetAxis("Horizontal") == 0)
{
upForce = Mathf.SmoothDamp(upForce, 0, ref refForce, 1f);
curRPM = Mathf.SmoothDamp(curRPM, 0, ref refRPM, 1 / Mathf.Pow(2, 0.5f));
}
}