HCW.SetReferenceOrbit(Spacecraft) Method

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Description

Sets the reference orbit of the HCW propagator by copying the current Keplerian state from the specified referenceSpacecraft. The reference orbit will be propagated with a two body (Keplerian) propagator when this Spacecraft is stepped.

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

HCW.SetReferenceOrbit(

Spacecraft referenceSpacecraft)

Arguments

referenceSpacecraft
Description:	The Spacecraft whose Keplerian state will be used to define the reference orbit.

Syntax

myHCW1.SetReferenceOrbit(mySpacecraft1);