本文整理汇总了C#中Orbit.TimeOfAscendingNode方法的典型用法代码示例。如果您正苦于以下问题：C# Orbit.TimeOfAscendingNode方法的具体用法？C# Orbit.TimeOfAscendingNode怎么用？C# Orbit.TimeOfAscendingNode使用的例子？那么, 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.TimeOfAscendingNode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: DeltaVAndTimeToMatchPlanesAscending
//Computes the delta-V and time of a burn to match planes with the target orbit. The output burnUT
//will be equal to the time of the first ascending node with respect to the target after the given UT.
//Throws an ArgumentException if o is hyperbolic and doesn't have an ascending node relative to the target.
public static Vector3d DeltaVAndTimeToMatchPlanesAscending(Orbit o, Orbit target, double UT, out double burnUT)
{
burnUT = o.TimeOfAscendingNode(target, UT);
Vector3d desiredHorizontal = Vector3d.Cross(target.SwappedOrbitNormal(), o.Up(burnUT));
Vector3d actualHorizontalVelocity = Vector3d.Exclude(o.Up(burnUT), o.SwappedOrbitalVelocityAtUT(burnUT));
Vector3d desiredHorizontalVelocity = actualHorizontalVelocity.magnitude * desiredHorizontal;
return desiredHorizontalVelocity - actualHorizontalVelocity;
}