//return the mass of the simulated FuelNode. This is not the same as the mass of the Part,
//because the simulated node may have lost resources, and thus mass, during the simulation.
public float Mass(int simStage)
{
//print("\n(" + simStage + ") " + partName.PadRight(25) + " dryMass " + dryMass.ToString("F3")
// + " ResMass " + (resources.Keys.Sum(id => resources[id] * MuUtils.ResourceDensity(id))).ToString("F3")
// + " Fairing Mass " + (inverseStage < simStage ? fairingMass : 0).ToString("F3")
// + " (" + fairingMass.ToString("F3") + ")"
// + " ModuleMass " + moduleMass.ToString("F3")
// );
return(dryMass + resources.Keys.Sum(id => resources[id] * MuUtils.ResourceDensity(id)) +
(inverseStage < simStage ? fairingMass : 0));
}
//return the mass of the simulated FuelNode. This is not the same as the mass of the Part,
//because the simulated node may have lost resources, and thus mass, during the simulation.
public double Mass(int simStage)
{
//print("\n(" + simStage + ") " + partName.PadRight(25) + " dryMass " + dryMass.ToString("F3")
// + " ResMass " + (resources.Keys.Sum(id => resources[id] * MuUtils.ResourceDensity(id))).ToString("F3")
// + " Fairing Mass " + (inverseStage < simStage ? fairingMass : 0).ToString("F3")
// + " (" + fairingMass.ToString("F3") + ")"
// + " ModuleMass " + moduleMass.ToString("F3")
// );
//return dryMass + resources.Keys.Sum(id => resources[id] * MuUtils.ResourceDensity(id)) +
double resMass = resources.KeysList.Slinq().Select((r, rs) => rs[r] * MuUtils.ResourceDensity(r), resources).Sum();
return(dryMass + resMass +
(inverseStage < simStage ? modulesUnstagedMass : modulesStagedMass));
}
public float moduleMass; // for debugging
public FuelNode(Part part, bool dVLinearThrust)
{
if (!part.IsLaunchClamp())
{
//print(part.partInfo.name.PadRight(25) + " " + part.mass.ToString("F4") + " " + part.GetPhysicslessChildMass().ToString("F4") + " " + part.GetModuleMass(part.partInfo.partPrefab.mass).ToString("F4"));
dryMass = part.mass; // Intentionally ignore the physic flag.
moduleMass = part.GetModuleMass(part.partInfo.partPrefab.mass);
if (part.HasModule <ModuleProceduralFairing>())
{
fairingMass = moduleMass;
}
}
inverseStage = part.inverseStage;
partName = part.partInfo.name;
//note which resources this part has stored
for (int i = 0; i < part.Resources.Count; i++)
{
PartResource r = part.Resources[i];
if (r.info.density > 0 && r.info.name != "IntakeAir")
{
if (r.flowState)
{
resources[r.info.id] = (float)r.amount;
}
else
{
dryMass += (float)(r.amount * r.info.density); // disabled resources are just dead weight
}
}
}
// TODO : handle the multiple active ModuleEngine case ( SXT engines with integrated vernier )
//record relevant engine stats
ModuleEngines engine = part.Modules.OfType <ModuleEngines>().FirstOrDefault(e => e.isEnabled);
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if ((HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || engine.getIgnitionState) && (engine.thrustPercentage > 0 || engine.minThrust > 0))
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = engine.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
for (int i = 0; i < engine.thrustTransforms.Count; i++)
{
thrust -= engine.thrustTransforms[i].forward / engine.thrustTransforms.Count;
}
Vector3d fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? EditorLogic.VesselRotation * Vector3d.up : engine.part.vessel.GetTransform().up;
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
thrustPercentage = engine.thrustPercentage;
minFuelFlow = engine.minFuelFlow;
maxFuelFlow = engine.maxFuelFlow;
atmosphereCurve = new FloatCurve(engine.atmosphereCurve.Curve.keys);
atmChangeFlow = engine.atmChangeFlow;
useAtmCurve = engine.useAtmCurve;
if (useAtmCurve)
{
atmCurve = new FloatCurve(engine.atmCurve.Curve.keys);
}
useVelCurve = engine.useVelCurve;
if (useAtmCurve)
{
velCurve = new FloatCurve(engine.velCurve.Curve.keys);
}
propellantSumRatioTimesDensity = engine.propellants.Where(prop => !prop.ignoreForIsp).Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = engine.propellants.Where(prop => MuUtils.ResourceDensity(prop.id) > 0 && !prop.ignoreForIsp).ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
}
public string partName; //for debugging
public FuelNode(Part part, bool dVLinearThrust)
{
if (part.IsPhysicallySignificant())
{
dryMass = part.mass;
}
inverseStage = part.inverseStage;
partName = part.partInfo.name;
//note which resources this part has stored
foreach (PartResource r in part.Resources)
{
if (r.info.density > 0 && r.name != "IntakeAir")
{
if (r.flowState)
{
resources[r.info.id] = (float)r.amount;
}
else
{
dryMass += (float)(r.amount * r.info.density); // disabled resources are just dead weight
}
}
}
//record relevant engine stats
ModuleEngines engine = part.Modules.OfType <ModuleEngines>().FirstOrDefault();
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if ((HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || engine.getIgnitionState) && engine.thrustPercentage > 0)
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = engine.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
foreach (var t in engine.thrustTransforms)
{
thrust -= t.forward / engine.thrustTransforms.Count;
}
Vector3 fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? Vector3d.up : (HighLogic.LoadedScene == GameScenes.SPH ? Vector3d.forward : (Vector3d)engine.part.vessel.GetTransform().up);
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
maxThrust = engine.thrustPercentage / 100f * engine.maxThrust;
if (part.IsMFE())
{
correctThrust = true;
if (HighLogic.LoadedSceneIsFlight && engine.realIsp > 0.0f)
{
maxThrust = maxThrust * engine.atmosphereCurve.Evaluate(0) / engine.realIsp; //engine.atmosphereCurve.Evaluate((float)FlightGlobals.ActiveVessel.atmDensity);
}
}
else
{
correctThrust = false;
}
ispCurve = engine.atmosphereCurve;
propellantSumRatioTimesDensity = engine.propellants.Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = engine.propellants.Where(prop => MuUtils.ResourceDensity(prop.id) > 0 && prop.name != "IntakeAir").ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
// And do the same for ModuleEnginesFX :(
ModuleEnginesFX enginefx = part.Modules.OfType <ModuleEnginesFX>().FirstOrDefault(e => e.isEnabled);
if (enginefx != null)
{
//Only count engines that either are ignited or will ignite in the future:
if ((HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || enginefx.getIgnitionState) && enginefx.thrustPercentage > 0)
{
//if an engine has been activated early, pretend it is in the current stage:
if (enginefx.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = enginefx.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
foreach (var t in enginefx.thrustTransforms)
{
thrust -= t.forward / enginefx.thrustTransforms.Count;
}
Vector3 fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? Vector3d.up : (HighLogic.LoadedScene == GameScenes.SPH ? Vector3d.forward : (Vector3d)enginefx.part.vessel.GetTransform().up);
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
maxThrust = enginefx.thrustPercentage / 100f * enginefx.maxThrust;
if (part.IsMFE())
{
correctThrust = true;
if (HighLogic.LoadedSceneIsFlight && enginefx.realIsp > 0.0f)
{
maxThrust = maxThrust * enginefx.atmosphereCurve.Evaluate(0) / enginefx.realIsp; //engine.atmosphereCurve.Evaluate((float)FlightGlobals.ActiveVessel.atmDensity);
}
}
else
{
correctThrust = false;
}
ispCurve = enginefx.atmosphereCurve;
propellantSumRatioTimesDensity = enginefx.propellants.Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = enginefx.propellants.Where(prop => PartResourceLibrary.Instance.GetDefinition(prop.id).density > 0 && prop.name != "IntakeAir").ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
}
public string partName; //for debugging
public FuelNode(Part part, bool dVLinearThrust)
{
if (part.IsPhysicallySignificant())
{
dryMass = part.mass;
}
inverseStage = part.inverseStage;
isFuelLine = (part is FuelLine);
isSepratron = part.IsSepratron();
partName = part.partInfo.name;
//note which resources this part has stored
foreach (PartResource r in part.Resources)
{
if (r.info.density > 0 && r.name != "IntakeAir")
{
resources[r.info.id] = (float)r.amount;
}
resourcesUnobtainableFromParent.Add(r.info.id);
}
//record relevant engine stats
ModuleEngines engine = part.Modules.OfType <ModuleEngines>().FirstOrDefault();
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if (HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || engine.getIgnitionState)
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = engine.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
foreach (var t in engine.thrustTransforms)
{
thrust -= t.forward / engine.thrustTransforms.Count;
}
Vector3 fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? Vector3d.up : (HighLogic.LoadedScene == GameScenes.SPH ? Vector3d.forward : (Vector3d)engine.part.vessel.GetTransform().up);
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
maxThrust = engine.thrustPercentage / 100f * engine.maxThrust;
if (part.Modules.Contains("ModuleEngineConfigs") || part.Modules.Contains("ModuleHybridEngine") || part.Modules.Contains("ModuleHybridEngines"))
{
correctThrust = true;
if (HighLogic.LoadedSceneIsFlight && engine.realIsp > 0.0f)
{
maxThrust = maxThrust * engine.atmosphereCurve.Evaluate(0) / engine.realIsp; //engine.atmosphereCurve.Evaluate((float)FlightGlobals.ActiveVessel.atmDensity);
}
}
else
{
correctThrust = false;
}
ispCurve = engine.atmosphereCurve;
propellantSumRatioTimesDensity = engine.propellants.Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = engine.propellants.Where(prop => PartResourceLibrary.Instance.GetDefinition(prop.id).density > 0 && prop.name != "IntakeAir").ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
// And do the same for ModuleEnginesFX :(
ModuleEnginesFX enginefx = part.Modules.OfType <ModuleEnginesFX>().Where(e => e.isEnabled).FirstOrDefault();
if (enginefx != null)
{
//Only count engines that either are ignited or will ignite in the future:
if (HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || enginefx.getIgnitionState)
{
//if an engine has been activated early, pretend it is in the current stage:
if (enginefx.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = enginefx.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
foreach (var t in enginefx.thrustTransforms)
{
thrust -= t.forward / enginefx.thrustTransforms.Count;
}
Vector3 fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? Vector3d.up : (HighLogic.LoadedScene == GameScenes.SPH ? Vector3d.forward : (Vector3d)enginefx.part.vessel.GetTransform().up);
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
maxThrust = enginefx.thrustPercentage / 100f * enginefx.maxThrust;
if (part.Modules.Contains("ModuleEngineConfigs") || part.Modules.Contains("ModuleHybridEngine") || part.Modules.Contains("ModuleHybridEngines"))
{
correctThrust = true;
if (HighLogic.LoadedSceneIsFlight && enginefx.realIsp > 0.0f)
{
maxThrust = maxThrust * enginefx.atmosphereCurve.Evaluate(0) / enginefx.realIsp; //engine.atmosphereCurve.Evaluate((float)FlightGlobals.ActiveVessel.atmDensity);
}
}
else
{
correctThrust = false;
}
ispCurve = enginefx.atmosphereCurve;
propellantSumRatioTimesDensity = enginefx.propellants.Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = enginefx.propellants.Where(prop => PartResourceLibrary.Instance.GetDefinition(prop.id).density > 0 && prop.name != "IntakeAir").ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
//figure out when this part gets decoupled. We do this by looking through this part and all this part's ancestors
//and noting which one gets decoupled earliest (i.e., has the highest inverseStage). Some parts never get decoupled
//and these are assigned decoupledInStage = -1.
decoupledInStage = -1;
Part p = part;
while (true)
{
if (p.IsDecoupler() || p.IsLaunchClamp())
{
if (p.inverseStage > decoupledInStage)
{
decoupledInStage = p.inverseStage;
}
}
if (p.parent == null)
{
break;
}
else
{
p = p.parent;
}
}
}
public string partName; //for debugging
public FuelNode(Part part)
{
bool physicallySignificant = (part.physicalSignificance != Part.PhysicalSignificance.NONE);
if (part.HasModule <ModuleLandingGear>() || part.HasModule <LaunchClamp>())
{
//Landing gear set physicalSignificance = NONE when they enter the flight scene
//Launch clamp mass should be ignored.
physicallySignificant = false;
}
if (physicallySignificant)
{
dryMass = part.mass;
}
inverseStage = part.inverseStage;
isFuelLine = (part is FuelLine);
isSepratron = part.IsSepratron();
partName = part.partInfo.name;
//note which resources this part has stored
foreach (PartResource r in part.Resources)
{
if (r.info.name != "ElectricCharge")
{
resources[r.info.id] = (float)r.amount;
}
resourcesUnobtainableFromParent.Add(r.info.id);
}
//record relevant engine stats
ModuleEngines engine = part.Modules.OfType <ModuleEngines>().FirstOrDefault();
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if (HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || engine.getIgnitionState)
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
maxThrust = engine.maxThrust;
ispCurve = engine.atmosphereCurve;
propellantSumRatioTimesDensity = engine.propellants.Sum(prop => prop.ratio * MuUtils.ResourceDensity(prop.id));
propellantRatios = engine.propellants.Where(prop => prop.name != "ElectricCharge").ToDictionary(prop => prop.id, prop => prop.ratio);
}
}
//figure out when this part gets decoupled. We do this by looking through this part and all this part's ancestors
//and noting which one gets decoupled earliest (i.e., has the highest inverseStage). Some parts never get decoupled
//and these are assigned decoupledInStage = -1.
decoupledInStage = -1;
Part p = part;
while (true)
{
if (p.IsDecoupler())
{
if (p.inverseStage > decoupledInStage)
{
decoupledInStage = p.inverseStage;
}
}
if (p.parent == null)
{
break;
}
else
{
p = p.parent;
}
}
}
private void Init(Part part, bool dVLinearThrust)
{
resources.Clear();
resourceConsumptions.Clear();
resourceDrains.Clear();
freeResources.Clear();
propellantRatios.Clear();
propellantFlows.Clear();
crossfeedSources.Clear();
isEngine = false;
dryMass = 0;
modulesStagedMass = 0;
decoupledInStage = int.MinValue;
modulesUnstagedMass = 0;
if (!part.IsLaunchClamp())
{
dryMass = part.prefabMass; // Intentionally ignore the physic flag.
modulesUnstagedMass = part.GetModuleMassNoAlloc((float)dryMass, ModifierStagingSituation.UNSTAGED);
modulesStagedMass = part.GetModuleMassNoAlloc((float)dryMass, ModifierStagingSituation.STAGED);
float currentModulesMass = part.GetModuleMassNoAlloc((float)dryMass, ModifierStagingSituation.CURRENT);
// if it was manually staged
if (currentModulesMass == modulesStagedMass)
{
modulesUnstagedMass = modulesStagedMass;
}
//print(part.partInfo.name.PadRight(25) + " " + part.mass.ToString("F4") + " " + part.GetPhysicslessChildMass().ToString("F4") + " " + modulesUnstagedMass.ToString("F4") + " " + modulesStagedMass.ToString("F4"));
}
inverseStage = part.inverseStage;
partName = part.partInfo.name;
resourceRequestRemainingThreshold = Math.Max(part.resourceRequestRemainingThreshold, DRAINED);
resourcePriority = part.GetResourcePriority();
//note which resources this part has stored
for (int i = 0; i < part.Resources.Count; i++)
{
PartResource r = part.Resources[i];
if (r.info.density > 0)
{
if (r.flowState)
{
resources[r.info.id] = r.amount;
}
else
{
dryMass += (r.amount * r.info.density); // disabled resources are just dead weight
}
}
if (r.info.name == "IntakeAir")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeAir").id] = true;
}
// Those two are in the CRP.
if (r.info.name == "IntakeLqd")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeLqd").id] = true;
}
if (r.info.name == "IntakeAtm")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeAtm").id] = true;
}
}
// TODO : handle the multiple active ModuleEngine case ( SXT engines with integrated vernier )
//record relevant engine stats
//ModuleEngines engine = part.Modules.OfType<ModuleEngines>().FirstOrDefault(e => e.isEnabled);
ModuleEngines engine = null;
for (int i = 0; i < part.Modules.Count; i++)
{
PartModule pm = part.Modules[i];
ModuleEngines e = pm as ModuleEngines;
if (e != null && e.isEnabled)
{
engine = e;
break;
}
}
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if ((HighLogic.LoadedSceneIsEditor || inverseStage < StageManager.CurrentStage || engine.getIgnitionState) && (engine.thrustPercentage > 0 || engine.minThrust > 0))
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < StageManager.CurrentStage)
{
inverseStage = StageManager.CurrentStage;
}
isEngine = true;
g = engine.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3.zero;
for (int i = 0; i < engine.thrustTransforms.Count; i++)
{
thrust -= engine.thrustTransforms[i].forward * engine.thrustTransformMultipliers[i];
}
Vector3d fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? EditorLogic.VesselRotation * Vector3d.up : engine.part.vessel.GetTransform().up;
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
else
{
fwdThrustRatio = 1;
}
thrustPercentage = engine.thrustPercentage;
minFuelFlow = engine.minFuelFlow;
maxFuelFlow = engine.maxFuelFlow;
// Some brilliant engine mod seems to consider that FuelFlow is not something they should properly initialize
if (minFuelFlow == 0 && engine.minThrust > 0)
{
maxFuelFlow = engine.minThrust / (engine.atmosphereCurve.Evaluate(0f) * engine.g);
}
if (maxFuelFlow == 0 && engine.maxThrust > 0)
{
maxFuelFlow = engine.maxThrust / (engine.atmosphereCurve.Evaluate(0f) * engine.g);
}
atmosphereCurve = new FloatCurve(engine.atmosphereCurve.Curve.keys);
atmChangeFlow = engine.atmChangeFlow;
useAtmCurve = engine.useAtmCurve;
if (useAtmCurve)
{
atmCurve = new FloatCurve(engine.atmCurve.Curve.keys);
}
useVelCurve = engine.useVelCurve;
if (useVelCurve)
{
velCurve = new FloatCurve(engine.velCurve.Curve.keys);
}
propellantSumRatioTimesDensity = engine.propellants.Slinq().Where(prop => !prop.ignoreForIsp).Select(prop => prop.ratio * MuUtils.ResourceDensity(prop.id)).Sum();
propellantRatios.Clear();
propellantFlows.Clear();
var dics = new Tuple <KeyableDictionary <int, float>, KeyableDictionary <int, ResourceFlowMode> >(propellantRatios, propellantFlows);
engine.propellants.Slinq()
.Where(prop => MuUtils.ResourceDensity(prop.id) > 0 && !prop.ignoreForIsp)
.ForEach((p, dic) =>
{
dic.Item1.Add(p.id, p.ratio);
dic.Item2.Add(p.id, p.GetFlowMode());
}, dics);
}
}
}
private void Init(Part part, bool dVLinearThrust)
{
resources.Clear();
resourceConsumptions.Clear();
resourceDrains.Clear();
freeResources.Clear();
propellantRatios.Clear();
propellantFlows.Clear();
fuelLineSources.Clear();
stackNodeSources.Clear();
surfaceMountSources.Clear();
surfaceMountParent = null;
isEngine = false;
dryMass = 0;
fairingMass = 0;
moduleMass = 0;
if (!part.IsLaunchClamp())
{
//print(part.partInfo.name.PadRight(25) + " " + part.mass.ToString("F4") + " " + part.GetPhysicslessChildMass().ToString("F4") + " " + part.GetModuleMass(part.partInfo.partPrefab.mass).ToString("F4"));
dryMass = part.mass; // Intentionally ignore the physic flag.
moduleMass = part.GetModuleMass(part.partInfo.partPrefab != null ? part.partInfo.partPrefab.mass : dryMass);
if (part.HasModule <ModuleProceduralFairing>())
{
fairingMass = moduleMass;
}
}
inverseStage = part.inverseStage;
partName = part.partInfo.name;
//note which resources this part has stored
for (int i = 0; i < part.Resources.Count; i++)
{
PartResource r = part.Resources[i];
if (r.info.density > 0)
{
if (r.flowState)
{
resources[r.info.id] = (float)r.amount;
}
else
{
dryMass += (float)(r.amount * r.info.density); // disabled resources are just dead weight
}
}
if (r.info.name == "IntakeAir")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeAir").id] = true;
}
// Those two are in the CRP.
if (r.info.name == "IntakeLqd")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeLqd").id] = true;
}
if (r.info.name == "IntakeAtm")
{
freeResources[PartResourceLibrary.Instance.GetDefinition("IntakeAtm").id] = true;
}
}
// TODO : handle the multiple active ModuleEngine case ( SXT engines with integrated vernier )
//record relevant engine stats
//ModuleEngines engine = part.Modules.OfType<ModuleEngines>().FirstOrDefault(e => e.isEnabled);
ModuleEngines engine = null;
for (int i = 0; i < part.Modules.Count; i++)
{
PartModule pm = part.Modules[i];
ModuleEngines e = pm as ModuleEngines;
if (e != null && e.isEnabled)
{
engine = e;
break;
}
}
if (engine != null)
{
//Only count engines that either are ignited or will ignite in the future:
if ((HighLogic.LoadedSceneIsEditor || inverseStage < Staging.CurrentStage || engine.getIgnitionState) && (engine.thrustPercentage > 0 || engine.minThrust > 0))
{
//if an engine has been activated early, pretend it is in the current stage:
if (engine.getIgnitionState && inverseStage < Staging.CurrentStage)
{
inverseStage = Staging.CurrentStage;
}
isEngine = true;
g = engine.g;
// If we take into account the engine rotation
if (dVLinearThrust)
{
Vector3 thrust = Vector3d.zero;
for (int i = 0; i < engine.thrustTransforms.Count; i++)
{
thrust -= engine.thrustTransforms[i].forward / engine.thrustTransforms.Count;
}
Vector3d fwd = HighLogic.LoadedScene == GameScenes.EDITOR ? EditorLogic.VesselRotation * Vector3d.up : engine.part.vessel.GetTransform().up;
fwdThrustRatio = Vector3.Dot(fwd, thrust);
}
else
{
fwdThrustRatio = 1;
}
thrustPercentage = engine.thrustPercentage;
minFuelFlow = engine.minFuelFlow;
maxFuelFlow = engine.maxFuelFlow;
atmosphereCurve = new FloatCurve(engine.atmosphereCurve.Curve.keys);
atmChangeFlow = engine.atmChangeFlow;
useAtmCurve = engine.useAtmCurve;
if (useAtmCurve)
{
atmCurve = new FloatCurve(engine.atmCurve.Curve.keys);
}
useVelCurve = engine.useVelCurve;
if (useVelCurve)
{
velCurve = new FloatCurve(engine.velCurve.Curve.keys);
}
propellantSumRatioTimesDensity = engine.propellants.Slinq().Where(prop => !prop.ignoreForIsp).Select(prop => prop.ratio * MuUtils.ResourceDensity(prop.id)).Sum();
propellantRatios.Clear();
propellantFlows.Clear();
var dics = new Tuple <KeyableDictionary <int, float>, KeyableDictionary <int, ResourceFlowMode> >(propellantRatios, propellantFlows);
engine.propellants.Slinq()
.Where(prop => MuUtils.ResourceDensity(prop.id) > 0 && !prop.ignoreForIsp)
.ForEach((p, dic) =>
{
dic._1.Add(p.id, p.ratio);
dic._2.Add(p.id, p.GetFlowMode());
}, dics);
}
}
}
