SpacecraftCovariance.GetCovarianceInFrame(CoordinateSystem) 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

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.GetCovarianceInFrame(

CoordinateSystem coordinate_system)

 

 

Arguments

coordinate_system

Description:

A CoordinateSystem to define the reference frame of the covariance.

 

 

 

Return Value

Type:

Matrix of number

 

 

The value of the converted Covariance matrix.

 

Syntax

myMatrix1 = mySpacecraftCovariance1.GetCovarianceInFrame(myCoordinateSystem1);

 

 

See also

SpacecraftCovariance Object

SpacecraftCovariance.GetCovarianceInFrame

Orbit Determination Guide