本文整理汇总了C#中Part.HasModule方法的典型用法代码示例。如果您正苦于以下问题：C# Part.HasModule方法的具体用法？C# Part.HasModule怎么用？C# Part.HasModule使用的例子？那么恭喜您, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类Part的用法示例。
在下文中一共展示了Part.HasModule方法的9个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C#代码示例。
示例1: FuelNode
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;
}
}示例2: New
public static PartSim New(Part p, int id, double atmosphere, LogMsg log)
{
PartSim partSim = pool.Borrow();
partSim.part = p;
partSim.centerOfMass = p.transform.TransformPoint(p.CoMOffset);
partSim.partId = id;
partSim.name = p.partInfo.name;
if (log != null) log.buf.AppendLine("Create PartSim for " + partSim.name);
partSim.parent = null;
partSim.parentAttach = p.attachMode;
partSim.fuelCrossFeed = p.fuelCrossFeed;
partSim.noCrossFeedNodeKey = p.NoCrossFeedNodeKey;
partSim.decoupledInStage = partSim.DecoupledInStage(p);
partSim.isFuelLine = p.HasModule<CModuleFuelLine>();
partSim.isFuelTank = p is FuelTank;
partSim.isSepratron = partSim.IsSepratron();
partSim.inverseStage = p.inverseStage;
//MonoBehaviour.print("inverseStage = " + inverseStage);
partSim.baseCost = p.GetCostDry();
if (log != null)
{
log.buf.AppendLine("Parent part = " + (p.parent == null ? "null" : p.parent.partInfo.name));
log.buf.AppendLine("physicalSignificance = " + p.physicalSignificance);
log.buf.AppendLine("PhysicsSignificance = " + p.PhysicsSignificance);
}
// Work out if the part should have no physical significance
// The root part is never "no physics"
partSim.isNoPhysics = p.physicalSignificance == Part.PhysicalSignificance.NONE ||
p.PhysicsSignificance == 1;
if (p.HasModule<LaunchClamp>())
{
partSim.realMass = 0d;
if (log != null) log.buf.AppendLine("Ignoring mass of launch clamp");
}
else
{
partSim.realMass = p.mass;
if (log != null) log.buf.AppendLine("Using part.mass of " + p.mass);
}
partSim.postStageMassAdjust = 0f;
if (log != null) log.buf.AppendLine("Calculating postStageMassAdjust, prefabMass = " + p.prefabMass);
int count = p.Modules.Count;
for (int i = 0; i < count; i++)
{
if (log != null) log.buf.AppendLine("Module: " + p.Modules[i].moduleName);
IPartMassModifier partMassModifier = p.Modules[i] as IPartMassModifier;
if (partMassModifier != null)
{
if (log != null) log.buf.AppendLine("ChangeWhen = " + partMassModifier.GetModuleMassChangeWhen());
if (partMassModifier.GetModuleMassChangeWhen() == ModifierChangeWhen.STAGED)
{
float preStage = partMassModifier.GetModuleMass(p.prefabMass, ModifierStagingSituation.UNSTAGED);
float postStage = partMassModifier.GetModuleMass(p.prefabMass, ModifierStagingSituation.STAGED);
if (log != null) log.buf.AppendLine("preStage = " + preStage + " postStage = " + postStage);
partSim.postStageMassAdjust += (postStage - preStage);
}
}
}
if (log != null) log.buf.AppendLine("postStageMassAdjust = " + partSim.postStageMassAdjust);
for (int i = 0; i < p.Resources.Count; i++)
{
PartResource resource = p.Resources[i];
// 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 (log != null)
log.buf.AppendLine(resource.resourceName + " = " + resource.amount);
partSim.resources.Add(resource.info.id, resource.amount);
partSim.resourceFlowStates.Add(resource.info.id, resource.flowState ? 1 : 0);
}
else
{
if (log != null) log.buf.AppendLine(resource.resourceName + " is NaN. Skipping.");
}
}
partSim.hasVessel = (p.vessel != null);
partSim.isLanded = partSim.hasVessel && p.vessel.Landed;
if (partSim.hasVessel)
{
partSim.vesselName = p.vessel.vesselName;
partSim.vesselType = p.vesselType;
}
partSim.initialVesselName = p.initialVesselName;
partSim.hasMultiModeEngine = p.HasModule<MultiModeEngine>();
partSim.hasModuleEngines = p.HasModule<ModuleEngines>();
//.........这里部分代码省略.........
示例3: PartSim
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;
parentAttach = part.attachMode;
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<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);
}示例4: IsDecoupler
private bool IsDecoupler(Part thePart)
{
return thePart.HasModule<ModuleDecouple>() ||
thePart.HasModule<ModuleAnchoredDecoupler>();
}示例5: IsFairing
private bool IsFairing(Part thePart)
{
return thePart.HasModule<ModuleProceduralFairing>();
}示例6: FuelNode
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 != 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 && 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);
}
}
}示例7: Init
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.GetModuleMassNoAlloc(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 < 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 = Vector3d.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);
//.........这里部分代码省略.........
示例8: IsARadialDecoupler
private static bool IsARadialDecoupler(Part part)
{
return part.HasModule<ModuleAnchoredDecoupler>() ||
part.FindModuleImplementing<ModuleDecouple>()?.explosiveNodeID == "srf";
}示例9: FuelNode
public FuelNode(Part part, bool dVLinearThrust)
{
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.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;
// 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;
// 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);
//.........这里部分代码省略.........