| public Add ( int type, double amount ) : void | ||
| type | int | |
| amount | double | |
| return | void | |
private void SetResourceDrainRateRecursive(int type, double amount, List <PartSim> visited = null)
{
if (visited == null)
{
visited = new List <PartSim>();
}
List <PartSim> newVisited = new List <PartSim>(visited);
newVisited.Add(this);
List <PartSim> fuelLines = new List <PartSim>();
foreach (PartSim partSim in sourceParts)
{
if (partSim.part is FuelLine && !visited.Contains(partSim))
{
if (partSim.CanSupplyResourceRecursive(type, newVisited))
{
fuelLines.Add(partSim);
}
}
}
if (fuelLines.Count > 0)
{
foreach (PartSim fuelLine in fuelLines)
{
fuelLine.SetResourceDrainRateRecursive(type, amount / fuelLines.Count, newVisited);
}
return;
}
foreach (PartSim partSim in sourceParts)
{
if (!visited.Contains(partSim) && partSim.CanSupplyResourceRecursive(type, newVisited))
{
if (DrainFromSourceBeforeSelf(type, partSim))
{
partSim.SetResourceDrainRateRecursive(type, amount, newVisited);
return;
}
}
}
if (this.resources[type] > 0)
{
resourceDrains.Add(type, amount);
}
}
public PartSim(Part thePart, int id, double atmosphere, LogMsg log)
{
part = thePart;
partId = id;
name = part.partInfo.name;
if (log != null)
{
log.buf.AppendLine("Create PartSim for " + name);
}
parent = null;
fuelCrossFeed = part.fuelCrossFeed;
noCrossFeedNodeKey = part.NoCrossFeedNodeKey;
decoupledInStage = DecoupledInStage(part);
isFuelLine = part is FuelLine;
isFuelTank = part is FuelTank;
isSepratron = IsSepratron();
inverseStage = part.inverseStage;
//MonoBehaviour.print("inverseStage = " + inverseStage);
cost = part.partInfo.cost;
foreach (PartResource resource in part.Resources)
{
cost -= (float)((resource.maxAmount - resource.amount) * resource.info.unitCost);
}
// Work out if the part should have no physical significance
isNoPhysics = part.HasModule <ModuleLandingGear>() ||
part.HasModule <LaunchClamp>() ||
part.physicalSignificance == Part.PhysicalSignificance.NONE ||
part.PhysicsSignificance == 1;
if (!isNoPhysics)
{
baseMass = part.mass;
}
if (SimManager.logOutput)
{
MonoBehaviour.print((isNoPhysics ? "Ignoring" : "Using") + " part.mass of " + part.mass);
}
foreach (PartResource resource in part.Resources)
{
// Make sure it isn't NaN as this messes up the part mass and hence most of the values
// This can happen if a resource capacity is 0 and tweakable
if (!Double.IsNaN(resource.amount))
{
if (SimManager.logOutput)
{
MonoBehaviour.print(resource.resourceName + " = " + resource.amount);
}
resources.Add(resource.info.id, resource.amount);
resourceFlowStates.Add(resource.info.id, resource.flowState ? 1 : 0);
}
else
{
MonoBehaviour.print(resource.resourceName + " is NaN. Skipping.");
}
}
startMass = GetMass();
hasVessel = (part.vessel != null);
isLanded = hasVessel && part.vessel.Landed;
if (hasVessel)
{
vesselName = part.vessel.vesselName;
vesselType = part.vesselType;
}
initialVesselName = part.initialVesselName;
hasMultiModeEngine = part.HasModule <MultiModeEngine>();
hasModuleEnginesFX = part.HasModule <ModuleEnginesFX>();
hasModuleEngines = part.HasModule <ModuleEngines>();
isEngine = hasMultiModeEngine || hasModuleEnginesFX || hasModuleEngines;
if (SimManager.logOutput)
{
MonoBehaviour.print("Created " + name + ". Decoupled in stage " + decoupledInStage);
}
}
public void SetResourceConsumptions()
{
if (this.part.HasModule <MultiModeEngine>())
{
string mode = this.part.GetModule <MultiModeEngine>().mode;
foreach (ModuleEnginesFX engine in this.part.GetModules <ModuleEnginesFX>())
{
if (engine.engineID == mode)
{
double flowRate = 0d;
if (part.vessel != null)
{
if (engine.throttleLocked)
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
else
{
if (part.vessel.Landed)
{
flowRate = Math.Max(0.000001d, engine.maxThrust * (engine.thrustPercentage / 100f) * FlightInputHandler.state.mainThrottle) / (isp * 9.81d);
}
else
{
if (engine.requestedThrust > 0)
{
flowRate = engine.requestedThrust / (isp * 9.81d);
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
}
}
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
float flowMass = 0f;
foreach (Propellant propellant in engine.propellants)
{
flowMass += propellant.ratio * ResourceContainer.GetResourceDensity(propellant.id);
}
foreach (Propellant propellant in engine.propellants)
{
if (propellant.name == "ElectricCharge" || propellant.name == "IntakeAir")
{
continue;
}
double consumptionRate = propellant.ratio * flowRate / flowMass;
resourceConsumptions.Add(propellant.id, consumptionRate);
}
}
}
}
else if (this.part.HasModule <ModuleEnginesFX>())
{
foreach (ModuleEnginesFX engine in part.GetModules <ModuleEnginesFX>())
{
double flowRate = 0d;
if (part.vessel != null)
{
if (engine.throttleLocked)
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
else
{
if (part.vessel.Landed)
{
flowRate = Math.Max(0.000001d, engine.maxThrust * (engine.thrustPercentage / 100f) * FlightInputHandler.state.mainThrottle) / (isp * 9.81d);
}
else
{
if (engine.requestedThrust > 0)
{
flowRate = engine.requestedThrust / (isp * 9.81d);
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
}
}
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
float flowMass = 0f;
foreach (Propellant propellant in engine.propellants)
{
flowMass += propellant.ratio * ResourceContainer.GetResourceDensity(propellant.id);
}
foreach (Propellant propellant in engine.propellants)
{
if (propellant.name == "ElectricCharge" || propellant.name == "IntakeAir")
{
continue;
}
double consumptionRate = propellant.ratio * flowRate / flowMass;
resourceConsumptions.Add(propellant.id, consumptionRate);
}
}
}
else if (this.part.HasModule <ModuleEngines>())
{
foreach (ModuleEngines engine in part.GetModules <ModuleEngines>())
{
double flowRate = 0d;
if (part.vessel != null)
{
if (engine.throttleLocked)
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
else
{
if (part.vessel.Landed)
{
flowRate = Math.Max(0.000001d, engine.maxThrust * (engine.thrustPercentage / 100f) * FlightInputHandler.state.mainThrottle) / (isp * 9.81d);
}
else
{
if (engine.requestedThrust > 0)
{
flowRate = engine.requestedThrust / (isp * 9.81d);
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
}
}
}
else
{
flowRate = engine.maxThrust * (engine.thrustPercentage / 100f) / (isp * 9.81d);
}
float flowMass = 0f;
foreach (Propellant propellant in engine.propellants)
{
flowMass += propellant.ratio * ResourceContainer.GetResourceDensity(propellant.id);
}
foreach (Propellant propellant in engine.propellants)
{
if (propellant.name == "ElectricCharge" || propellant.name == "IntakeAir")
{
continue;
}
double consumptionRate = propellant.ratio * flowRate / flowMass;
resourceConsumptions.Add(propellant.id, consumptionRate);
}
}
}
}
public PartSim(Part part, double atmosphere)
{
this.part = part;
foreach (PartResource resource in part.Resources)
{
resources.Add(resource.info.id, resource.amount);
}
if (this.part.HasModule <MultiModeEngine>())
{
string mode = this.part.GetModule <MultiModeEngine>().mode;
foreach (ModuleEnginesFX engine in this.part.GetModules <ModuleEnginesFX>())
{
if (engine.engineID == mode)
{
if (part.vessel != null)
{
actualThrust = engine.requestedThrust;
isp = engine.atmosphereCurve.Evaluate((float)part.staticPressureAtm);
}
else
{
isp = engine.atmosphereCurve.Evaluate((float)atmosphere);
}
thrust = engine.maxThrust * (engine.thrustPercentage / 100f);
}
}
}
else if (this.part.HasModule <ModuleEnginesFX>())
{
foreach (ModuleEnginesFX engine in this.part.GetModules <ModuleEnginesFX>())
{
if (part.vessel != null)
{
actualThrust = engine.requestedThrust;
isp = engine.atmosphereCurve.Evaluate((float)part.staticPressureAtm);
}
else
{
isp = engine.atmosphereCurve.Evaluate((float)atmosphere);
}
thrust = engine.maxThrust * (engine.thrustPercentage / 100f);
}
}
else if (this.part.HasModule <ModuleEngines>())
{
foreach (ModuleEngines engine in this.part.GetModules <ModuleEngines>())
{
if (part.vessel != null)
{
actualThrust = engine.requestedThrust;
isp = engine.atmosphereCurve.Evaluate((float)part.staticPressureAtm);
}
else
{
isp = engine.atmosphereCurve.Evaluate((float)atmosphere);
}
thrust = engine.maxThrust * (engine.thrustPercentage / 100f);
}
}
decoupledInStage = DecoupledInStage();
}
public EngineSim(PartSim theEngine,
double atmosphere,
double velocity,
float maxThrust,
float minThrust,
float thrustPercentage,
float requestedThrust,
Vector3 vecThrust,
float realIsp,
FloatCurve atmosphereCurve,
FloatCurve velocityCurve,
bool throttleLocked,
List <Propellant> propellants,
bool active,
bool correctThrust)
{
StringBuilder buffer = null;
//MonoBehaviour.print("Create EngineSim for " + theEngine.name);
//MonoBehaviour.print("maxThrust = " + maxThrust);
//MonoBehaviour.print("minThrust = " + minThrust);
//MonoBehaviour.print("thrustPercentage = " + thrustPercentage);
//MonoBehaviour.print("requestedThrust = " + requestedThrust);
//MonoBehaviour.print("velocity = " + velocity);
partSim = theEngine;
isActive = active;
thrust = (maxThrust - minThrust) * (thrustPercentage / 100f) + minThrust;
//MonoBehaviour.print("thrust = " + thrust);
thrustVec = vecThrust;
double flowRate = 0d;
if (partSim.hasVessel)
{
//MonoBehaviour.print("hasVessel is true");
actualThrust = requestedThrust;
if (velocityCurve != null)
{
actualThrust *= velocityCurve.Evaluate((float)velocity);
//MonoBehaviour.print("actualThrust at velocity = " + actualThrust);
}
isp = atmosphereCurve.Evaluate((float)partSim.part.staticPressureAtm);
if (isp == 0d)
{
MonoBehaviour.print("Isp at " + partSim.part.staticPressureAtm + " is zero. Flow rate will be NaN");
}
if (correctThrust && realIsp == 0)
{
float ispsl = atmosphereCurve.Evaluate(0);
if (ispsl != 0)
{
thrust = thrust * isp / ispsl;
}
else
{
MonoBehaviour.print("Isp at sea level is zero. Unable to correct thrust.");
}
//MonoBehaviour.print("corrected thrust = " + thrust);
}
if (velocityCurve != null)
{
thrust *= velocityCurve.Evaluate((float)velocity);
//MonoBehaviour.print("thrust at velocity = " + thrust);
}
if (throttleLocked)
{
//MonoBehaviour.print("throttleLocked is true");
flowRate = thrust / (isp * 9.81d);
}
else
{
if (partSim.isLanded)
{
//MonoBehaviour.print("partSim.isLanded is true, mainThrottle = " + FlightInputHandler.state.mainThrottle);
flowRate = Math.Max(0.000001d, thrust * FlightInputHandler.state.mainThrottle) / (isp * 9.81d);
}
else
{
if (requestedThrust > 0)
{
if (velocityCurve != null)
{
requestedThrust *= velocityCurve.Evaluate((float)velocity);
//MonoBehaviour.print("requestedThrust at velocity = " + requestedThrust);
}
//MonoBehaviour.print("requestedThrust > 0");
flowRate = requestedThrust / (isp * 9.81d);
}
else
{
//MonoBehaviour.print("requestedThrust <= 0");
flowRate = thrust / (isp * 9.81d);
}
}
}
}
else
{
//MonoBehaviour.print("hasVessel is false");
isp = atmosphereCurve.Evaluate((float)atmosphere);
if (isp == 0d)
{
MonoBehaviour.print("Isp at " + atmosphere + " is zero. Flow rate will be NaN");
}
if (correctThrust)
{
float ispsl = atmosphereCurve.Evaluate(0);
if (ispsl != 0)
{
thrust = thrust * isp / ispsl;
}
else
{
MonoBehaviour.print("Isp at sea level is zero. Unable to correct thrust.");
}
//MonoBehaviour.print("corrected thrust = " + thrust);
}
if (velocityCurve != null)
{
thrust *= velocityCurve.Evaluate((float)velocity);
//MonoBehaviour.print("thrust at velocity = " + thrust);
}
flowRate = thrust / (isp * 9.81d);
}
if (SimManager.logOutput)
{
buffer = new StringBuilder(1024);
buffer.AppendFormat("flowRate = {0:g6}\n", flowRate);
}
float flowMass = 0f;
foreach (Propellant propellant in propellants)
{
flowMass += propellant.ratio * ResourceContainer.GetResourceDensity(propellant.id);
}
if (SimManager.logOutput)
{
buffer.AppendFormat("flowMass = {0:g6}\n", flowMass);
}
foreach (Propellant propellant in propellants)
{
if (propellant.name == "ElectricCharge" || propellant.name == "IntakeAir")
{
continue;
}
double consumptionRate = propellant.ratio * flowRate / flowMass;
if (SimManager.logOutput)
{
buffer.AppendFormat("Add consumption({0}, {1}:{2:d}) = {3:g6}\n", ResourceContainer.GetResourceName(propellant.id), theEngine.name, theEngine.partId, consumptionRate);
}
resourceConsumptions.Add(propellant.id, consumptionRate);
}
if (SimManager.logOutput)
{
MonoBehaviour.print(buffer);
}
}