本文整理汇总了C#中Orbit.GetAngleToVector方法的典型用法代码示例。如果您正苦于以下问题：C# Orbit.GetAngleToVector方法的具体用法？C# Orbit.GetAngleToVector怎么用？C# Orbit.GetAngleToVector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Orbit的用法示例。
在下文中一共展示了Orbit.GetAngleToVector方法的1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: Update
/// <summary>
/// Updates the details by recalculating if requested.
/// </summary>
public void Update()
{
if (FlightGlobals.fetch == null ||
FlightGlobals.fetch.VesselTarget == null ||
FlightGlobals.ActiveVessel == null ||
FlightGlobals.ActiveVessel.targetObject == null ||
FlightGlobals.ActiveVessel.targetObject.GetOrbit() == null ||
FlightGlobals.ship_orbit == null ||
FlightGlobals.ship_orbit.referenceBody == null)
{
ShowDetails = false;
return;
}
ShowDetails = true;
targetOrbit = FlightGlobals.fetch.VesselTarget.GetOrbit();
originOrbit = (FlightGlobals.ship_orbit.referenceBody == Planetarium.fetch.Sun ||
FlightGlobals.ship_orbit.referenceBody == FlightGlobals.ActiveVessel.targetObject.GetOrbit().referenceBody)
? FlightGlobals.ship_orbit
: FlightGlobals.ship_orbit.referenceBody.orbit;
RelativeInclination = originOrbit.GetRelativeInclination(targetOrbit);
RelativeVelocity = FlightGlobals.ship_tgtSpeed;
RelativeSpeed = FlightGlobals.ship_obtSpeed - targetOrbit.orbitalSpeed;
PhaseAngle = originOrbit.GetPhaseAngle(targetOrbit);
InterceptAngle = CalcInterceptAngle();
TimeToAscendingNode = originOrbit.GetTimeToVector(GetAscendingNode());
TimeToDescendingNode = originOrbit.GetTimeToVector(GetDescendingNode());
AngleToAscendingNode = originOrbit.GetAngleToVector(GetAscendingNode());
AngleToDescendingNode = originOrbit.GetAngleToVector(GetDescendingNode());
AltitudeSeaLevel = targetOrbit.altitude;
ApoapsisHeight = targetOrbit.ApA;
PeriapsisHeight = targetOrbit.PeA;
TimeToApoapsis = targetOrbit.timeToAp;
TimeToPeriapsis = targetOrbit.timeToPe;
SemiMajorAxis = targetOrbit.semiMajorAxis;
SemiMinorAxis = targetOrbit.semiMinorAxis;
Distance = Vector3d.Distance(targetOrbit.pos, originOrbit.pos);
OrbitalPeriod = targetOrbit.period;
// beware that the order/sign of coordinates is inconsistent across different exposed variables
// in particular, v below does not equal to FlightGlobals.ship_tgtVelocity
Vector3d x = targetOrbit.pos - originOrbit.pos;
Vector3d v = targetOrbit.vel - originOrbit.vel;
double xv = Vector3d.Dot(x, v);
TimeToRendezvous = - xv / Vector3d.SqrMagnitude(v);
RelativeRadialVelocity = xv / Vector3d.Magnitude(x);
}