SpacecraftCovariance.GetCovarianceInFrame(String) Method

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Description

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

Timing Precision Mode

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SpacecraftCovariance.GetCovarianceInFrame(

String referenceFrame)

referenceFrame

Description:

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

Valid Values:

Type:

Matrix of number

The value of the converted Covariance matrix.

myMatrix1 = mySpacecraftCovariance1.GetCovarianceInFrame(myString1);