TrajectoryPhase.AddNodes Method

Signatures

Return Value

Description

TrajectoryPhase.AddNodes(Ephemeris ephemeris)

None

Uses the position, velocity, mass, and epoch data from the Ephemeris to create new TrajectoryNodes.

TrajectoryPhase.AddNodes(TrajectoryPhase phase)

None

Appends the TrajectoryNodes from the passed TrajectoryPhase to the calling TrajectoryPhase.

TrajectoryPhase.AddNodes(Spacecraft spacecraft, TimeSpan duration, Variable numberOfNodes, Variable resetSpacecraft)

None

Propagates the passed Spacecraft using its current Propagator for the passed duration and saves numberOfNodes equally spaced TrajectoryNodes during the propagation. If the resetSpacecraftState = 1, then the Spacecraft's state will be restored to its original state once this process is complete.