HCW.SetReferenceOrbit(Array) Method

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Description

Sets the reference orbit of the HCW propagator using the specified Keplerian orbital elements (A, E, I, RAAN, W, TA) with respect to the ICRF. 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 nanosecond timing precision mode.

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

Method Signature

HCW.SetReferenceOrbit(

Array referenceOrbit)

Arguments

referenceOrbit
Description:	The Array containing the reference orbit's Keplerian Elements (A, E, I, RAAN, W, TA).
Required Size:	6

Syntax

myHCW1.SetReferenceOrbit(myArray1);