SpacecraftCovariance.GetOrbitStateCovarianceInElementSet(String) Method

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Description

Returns the covariance of the orbit state in the specified element set.

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

 

Method Signature

SpacecraftCovariance.GetOrbitStateCovarianceInElementSet(

String elementSetToReturn)

 

Arguments

elementSetToReturn


Description:

Element set type to convert the covariance to.

Valid Values:

Value

Label

"Cartesian"

Cartesian

"Equinoctial"

Equinoctial

 

 

Return Value

Type:

Matrix of number

 

The value of the specified Covariance matrix element.

 

Syntax

myMatrix1 = mySpacecraftCovariance1.GetOrbitStateCovarianceInElementSet(myString1);

 

See also

SpacecraftCovariance Object

Defining the Element Set to Process

Orbit Determination Guide