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 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.

Click here to see the documentation for this object 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);