void updateAngularDrag()
{
_rigidbody.angularDrag = (Mathf.PI * _constval.GetC_AngularDrag() / 5f) * _constval.GetAirDensity()
* Mathf.Pow(rotationYVelocity, 2) * Mathf.Pow(((DroneWedth / 2f) + (DroneLength / 2f)) / 2f, 5) +
(Mathf.PI * _constval.GetC_AngularDrag() / 5f) * _constval.GetAirDensity()
* Mathf.Pow(tiltVelocityForward, 2) * Mathf.Pow(((DroneWedth / 2f) + (DroneLength / 2f)) / 2f, 5) +
(Mathf.PI * _constval.GetC_AngularDrag() / 5f) * _constval.GetAirDensity()
* Mathf.Pow(tiltVelocitySwerve, 2) * Mathf.Pow(((DroneWedth / 2f) + (DroneLength / 2f)) / 2f, 5);
}
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();
}
