TrajectoryPhase.AddNodes(Spacecraft, TimeSpan, Variable, Variable) Method

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Description

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.

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

Arguments

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

duration
Description:	The duration for the propagation.
Units:	day

numberOfNodes
Description:	The number of TrajectoryNodes to add.
Valid Range:	numberOfNodes ≥ 3

resetSpacecraft

Description:

Whether to return the spacecraft to its original state after adding nodes.

Valid Values:

Value	Label
0	false
1	true

Syntax

myTrajectoryPhase1.AddNodes(mySpacecraft1, myTimeSpan1, myVariable1, myVariable2);