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.

Click here to see the documentation for this object in millisecond 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