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.

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

 

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);

 

 

See also

SpacecraftCovariance Object

SpacecraftCovariance.GetSmoothedCovarianceInFrame

Orbit Determination Guide