TrajectoryPhase.AddNode(Spacecraft) Method

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Description

Adds a state to the underlying TrajectoryNodes of the TrajectoryPhase using the current state of the passed Spacecraft.

Note: if the Spacecraft's central body differs from the TrajectoryPhase's central body, a state conversion will take place automatically before the TrajectoryNode is added.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

Method Signature

TrajectoryPhase.AddNode(

Spacecraft spacecraft)

Arguments

spacecraft
Description:	The spacecraft to extract the position, velocity, mass, and epoch from for the new TrajectoryNode.

Syntax

myTrajectoryPhase1.AddNode(mySpacecraft1);