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 millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

Click here to see the documentation for this object in nanosecond 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);