BroadcastEphemeris(RinexNavFile, Variable) Constructor

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Description

Create a BroadcastEphemeris propagator using the specified RinexNavFile and numeric ID code. When no GNSS constellation is specified, GPS is assumed.

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.

Constructor Signature

BroadcastEphemeris(	RinexNavFile navFile,
	Variable id_number)

Arguments

navFile
Description:	The RinexNavFile object.

id_number
Description:	The numeric ID code of the GNSS spacecraft.
Valid Range:	id_number > 0

Syntax

BroadcastEphemeris myBroadcastEphemeris1(myRinexNavFile1, myVariable1);