void MovemenForward()
{
if (Input.GetAxis("Vertical") != 0)
{
Tor = (1f / (2 * Mathf.PI)) * _constval.GetC_Pow() * _constval.GetAirDensity()
* Mathf.Pow(rotationAmount, 2) * Mathf.Pow(_constval.GetPropellerDiameter(), 5) * Input.GetAxis("FlyUp");
_rigidbody.AddRelativeForce(Vector3.forward * upForce * Mathf.Abs(Mathf.Sin(_rigidbody.rotation.eulerAngles.x * Mathf.PI / 180))
* Input.GetAxis("Vertical"));
_rigidbody.AddRelativeTorque(Vector3.forward * Tor);
if (Input.GetAxis("Vertical") > 0)
{
tiltAmountForward = Mathf.SmoothDamp(tiltAmountForward, tiltAmount, ref tiltVelocityForward, 1f);
}
else if (Input.GetAxis("Vertical") < 0)
{
tiltAmountForward = Mathf.SmoothDamp(tiltAmountForward, -tiltAmount, ref tiltVelocityForward, 1f);
}
}
}
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();
}