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. 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.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 to the ICRF.

Syntax

mySpacecraftCovariance1.MapErrorEllipsoid(myArray1, myCoordinateSystem1);