SpacecraftCovariance.MapErrorEllipsoid(Array, CoordinateSystem) Method

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Description

Determines the orientation and size of the Error Ellipsoid by calculating the Eigenvalues and Eigenvectors of the 3x3 position Covariance.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

 

Method Signature

SpacecraftCovariance.MapErrorEllipsoid(

Array eigenValues,


CoordinateSystem dcm)

 

 

Arguments

eigenValues


Description:

A 3 element array containing the component Eigenvalues.

Required Size:

At least 3

 

 

dcm


Description:

A CoordinateSystem object to hold the orientation of the Error Ellipse, relative ot the MJ2000 reference frame.

 

 

 

Syntax

mySpacecraftCovariance1.MapErrorEllipsoid(myArray1, myCoordinateSystem1);

 

 

See also

SpacecraftCovariance Object

SpacecraftCovariance.MapErrorEllipsoid

Orbit Determination Guide