SpacecraftCovariance.GetSmoothedCovarianceInFrame(String) Method

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Description

Returns the smoothed covariance of the spacecraft state in the specified attitude reference frame. This method is only used with the Cartesian element set.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

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Method Signature

SpacecraftCovariance.GetSmoothedCovarianceInFrame(

String referenceFrame)

Arguments

referenceFrame

Description:

The attitude reference frame in which the smoothed covariance will be expressed.

Valid Values:

Value	Label
"ICRF"	ICRF
"VNB"	VNB
"LVLH"	LVLH
"GEODETIC"	GEODETIC
"UVW"	UVW
"RIC"	RIC

Return Value

Type:

Matrix of number

The value of the converted smoothed covariance matrix.

Syntax

myMatrix1 = mySpacecraftCovariance1.GetSmoothedCovarianceInFrame(myString1);