本文整理汇总了C#中Part.IsLaunchClamp方法的典型用法代码示例。如果您正苦于以下问题：C# Part.IsLaunchClamp方法的具体用法？C# Part.IsLaunchClamp怎么用？C# Part.IsLaunchClamp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.IsLaunchClamp方法的4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: AssignDecoupledInStage
// Determine when this part will be decoupled given when its parent will be decoupled.
// Then recurse to all of this part's children.
public void AssignDecoupledInStage(Part p, Dictionary<Part, FuelNode> nodeLookup, int parentDecoupledInStage)
{
if (p.IsUnfiredDecoupler() || p.IsLaunchClamp())
{
decoupledInStage = p.inverseStage > parentDecoupledInStage ? p.inverseStage : parentDecoupledInStage;
}
else
{
decoupledInStage = parentDecoupledInStage;
}
isSepratron = isEngine && (inverseStage == decoupledInStage);
for (int i = 0; i < p.children.Count; i++)
{
Part child = p.children[i];
nodeLookup[child].AssignDecoupledInStage(child, nodeLookup, decoupledInStage);
}
}示例2: 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3: 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4: AssignDecoupledInStage
//.........这里部分代码省略.........
{
attach = p.findAttachNode(mAnchoredDecoupler.explosiveNodeID);
}
else
{
attach = p.srfAttachNode;
}
if (attach != null && attach.attachedPart != null)
{
if (attach.attachedPart == p.parent)
{
isDecoupler = true;
// We are decoupling our parent
// The part and its children are not part of the ship when we decouple
decoupledInStage = p.inverseStage;
//print("AssignDecoupledInStage ModuleAnchoredDecoupler " + p.partInfo.name + "(" + p.inverseStage + ") decoupling " + attach.attachedPart + "(" + attach.attachedPart.inverseStage + "). parent " + decoupledInStage);
// The parent should already have its info assigned at this point
//nodeLookup[p.parent].AssignDecoupledInStage(p.parent, nodeLookup, p.inverseStage);
}
else
{
isDecoupler = true;
// We are still attached to our parent
// The part and it's children are dropped when the parent is
decoupledInStage = parentDecoupledInStage;
//print("AssignDecoupledInStage ModuleAnchoredDecoupler " + p.partInfo.name + "(" + p.inverseStage + ") decoupling " + attach.attachedPart + "(" + attach.attachedPart.inverseStage + "). not the parent " + decoupledInStage);
// The part we decouple is dropped when we decouple
nodeLookup[attach.attachedPart].AssignDecoupledInStage(attach.attachedPart, nodeLookup, p.inverseStage);
}
}
break;
}
}
ModuleDockingNode mDockingNode = m as ModuleDockingNode;
if (mDockingNode != null)
{
if (mDockingNode.staged && mDockingNode.stagingEnabled && p.stagingOn)
{
Part attachedPart = mDockingNode.referenceNode.attachedPart;
if (attachedPart != null)
{
if (attachedPart == p.parent)
{
isDecoupler = true;
// We are decoupling our parent
// The part and its children are not part of the ship when we decouple
decoupledInStage = p.inverseStage;
// The parent should already have its info assigned at this point
//nodeLookup[p.parent].AssignDecoupledInStage(p.parent, nodeLookup, p.inverseStage);
}
else
{
isDecoupler = true;
decoupledInStage = parentDecoupledInStage;
//childDecoupledInStage = parentDecoupledInStage;
nodeLookup[attachedPart].AssignDecoupledInStage(attachedPart, nodeLookup, p.inverseStage);
}
}
}
break;
}
if (m.moduleName == "ProceduralFairingDecoupler")
{
if (!m.Fields["decoupled"].GetValue<bool>(m) && m.stagingEnabled && p.stagingOn)
{
isDecoupler = true;
// We are decoupling our parent
// The part and its children are not part of the ship when we decouple
decoupledInStage = p.inverseStage;
break;
}
}
}
if (p.IsLaunchClamp())
{
decoupledInStage = p.inverseStage > parentDecoupledInStage ? p.inverseStage : parentDecoupledInStage;
//print("AssignDecoupledInStage D " + p.partInfo.name + " " + parentDecoupledInStage);
}
else if (!isDecoupler)
{
decoupledInStage = parentDecoupledInStage;
//print("AssignDecoupledInStage " + p.partInfo.name + "(" + p.inverseStage + ")" + decoupledInStage);
}
isSepratron = isEngine && (inverseStage == decoupledInStage);
for (int i = 0; i < p.children.Count; i++)
{
Part child = p.children[i];
nodeLookup[child].AssignDecoupledInStage(child, nodeLookup, decoupledInStage);
}
}