CelestialObject.SetCartesianState(Variable, Array) Method

Top

Description

Sets the Cartesian state of the CelestialObject in the ICRF, referenced from the CentralBody. This requires that the CelestialObject uses a TwoBody propagator, and will error if other propagators are used.

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

CelestialObject.SetCartesianState(	Variable epoch,
	Array state)

Arguments

epoch
Description:	The epoch at which the CelestialObject's state is evaluated.

state
Description:	array containing the Cartesian Elements
Required Size:	6

Syntax

myCelestialObject1.SetCartesianState(myVariable1, myArray1);