| public GetUllageState ( Color &col ) : string | ||
| col | Color | |
| return | string | |
public override void FixedUpdate()
{
if (HighLogic.LoadedSceneIsEditor)
{
if (ullageSet != null && pressureFed)
{
if (ullageSet.EditorPressurized()) // we need to recheck each frame. Expensive, but short of messages....
{
propellantStatus = "Feed pressure OK";
}
else
{
propellantStatus = "Feed pressure too low";
}
}
else
{
propellantStatus = "OK";
}
}
needSetPropStatus = true;
base.FixedUpdate();
if (needSetPropStatus && showPropStatus)
{
if (pressureFed && !ullageSet.PressureOK())
{
propellantStatus = "Feed pressure too low";
}
else if (ullage && RFSettings.Instance.simulateUllage)
{
propellantStatus = ullageSet.GetUllageState(out ullageColor);
part.stackIcon.SetIconColor(ullageColor);
}
else
{
propellantStatus = "Nominal";
}
}
}
public override void UpdateFlightCondition(EngineThermodynamics ambientTherm, double altitude, Vector3d vel, double mach, bool oxygen)
{
throttledUp = false;
// handle ignition
if (HighLogic.LoadedSceneIsFlight)
{
if (vessel.ctrlState.mainThrottle > 0f || throttleLocked)
{
throttledUp = true;
}
else
{
ignited = false;
}
IgnitionUpdate();
// Ullage
bool pressureOK = ullageSet.PressureOK();
propellantStatus = "Nominal";
if (ullage)
{
propellantStatus = ullageSet.GetUllageState();
if (EngineIgnited && ignited && throttledUp)
{
double state = ullageSet.GetUllageStability();
double testValue = Math.Pow(state, RFSettings.Instance.stabilityPower);
if (UnityEngine.Random.value > testValue)
{
ScreenMessages.PostScreenMessage(ullageFail);
FlightLogger.eventLog.Add("[" + FormatTime(vessel.missionTime) + "] " + ullageFail.message);
reignitable = false;
ullageOK = false;
ignited = false;
Flameout("Vapor in feed line");
}
}
}
if (!pressureOK)
{
ignited = false;
reignitable = false;
propellantStatus = "Feed pressure too low"; // override ullage status indicator
Flameout("Lack of pressure");
}
rfSolver.SetEngineStatus(pressureOK, ullageOK, ignited);
// do thrust curve
if (ignited && useThrustCurve)
{
thrustCurveRatio = (float)((propellants[curveProp].totalResourceAvailable / propellants[curveProp].totalResourceCapacity));
if (thrustCurveUseTime)
{
thrustCurveDisplay = thrustCurve.Evaluate(curveTime);
if (EngineIgnited)
{
curveTime += TimeWarp.fixedDeltaTime;
}
}
else
{
thrustCurveDisplay = thrustCurve.Evaluate(thrustCurveRatio);
}
rfSolver.UpdateThrustRatio(thrustCurveDisplay);
thrustCurveDisplay *= 100f;
}
}
// Set part temp
rfSolver.SetPartTemp(part.temperature);
// do heat
heatProduction = (float)(scaleRecip * extHeatkW / PhysicsGlobals.InternalHeatProductionFactor * part.thermalMassReciprocal);
// run base method code
base.UpdateFlightCondition(ambientTherm, altitude, vel, mach, oxygen);
}
