AirControl.AC_Airplane_Engine Class Reference

Engine controls More...

Inheritance diagram for AirControl.AC_Airplane_Engine:

Collaboration diagram for AirControl.AC_Airplane_Engine:

Public Member Functions
void	getAngularVelocityPro ()
Vector3	CalculateForce (float throttle)
	Calculate the force created by engine Calculate Engine RPM Calculate fuel consumption More...

Public Attributes
float	maxForce = 3000f
float	maxRPM = 3500f
AnimationCurve	powerCurve = AnimationCurve.Linear(0f, 0f, 1f, 1f)
AnimationCurve	liftOff = AnimationCurve.Linear(0f, 0f, 1000f, 1000f)
AC_Airplane_Propeller	propeller

Properties
bool	ShutEngineOff [set]
float	CurrentRPM [get]

Detailed Description

Engine controls

Definition at line 22 of file AC_Airplane_Engine.cs.

Member Function Documentation

CalculateForce()

Vector3 AirControl.AC_Airplane_Engine.CalculateForce ( float  throttle )

inline

Calculate the force created by engine Calculate Engine RPM Calculate fuel consumption

Parameters

throttle

Input throttle value

Returns

Final Engine force

Definition at line 110 of file AC_Airplane_Engine.cs.

        {
            //Calcualte Power
            float finalThrottle = Mathf.Clamp01(throttle);
            // angular velocity
            getAngularVelocityPro();
 
            if(!isShutOff)
            {
                finalThrottle = powerCurve.Evaluate(finalThrottle);
                //keep eye on last throttle value, In case of engine cutoff we can use this value to slowly decrease the engine power
                lastThrottleValue = finalThrottle;
            }
            else
            {
                lastThrottleValue -= Time.deltaTime * shutOffSpeed;
                lastThrottleValue = Mathf.Clamp01(lastThrottleValue);
                finalThrottle = powerCurve.Evaluate(lastThrottleValue);
            }
 
 
            //Calculate RPM's
            currentRPM = finalThrottle * maxRPM;
            if(propeller)
            {
                propeller.HandlePropeller(currentRPM);
            }
 
 
            // Process the Fuel
            HandleFuel(finalThrottle);
 
 
            //Create Force
            float finalPower = finalThrottle * maxForce;
            Vector3 finalForce = transform.forward * finalPower;
 
            #region DBArea
            //Setting Current engine paramters to DB
            // DB_Functions.SetEngineVariables(connection, maxForce, finalPower,  maxRPM, CurrentRPM);
            StaticOutputSchema.MaxPower = maxForce; // can be moved to start
            StaticOutputSchema.CurrentPower = finalPower;
            StaticOutputSchema.MaxRPM = maxRPM; // can be moved to start
            StaticOutputSchema.CurrentRPM = currentRPM;
            #endregion
 
            return finalForce;
        }

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The documentation for this class was generated from the following file:

• AC_Airplane_Engine.cs