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 nanosecond timing precision mode.
Click here to see the documentation for this object in millisecond timing precision mode.
Method Signature
SpacecraftCovariance.MapErrorEllipsoid(
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Array eigenValues,
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Array eigenVector1,
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Array eigenVector2,
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Array eigenVector3)
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Arguments
eigenValues
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Description:
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A 3 element array containing the component Eigenvalues.
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Required Size:
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At least 3
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eigenVector1
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Description:
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A 3 element array containing the first component Eigenvector.
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Required Size:
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At least 3
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eigenVector2
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Description:
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A 3 element array containing the second component Eigenvector.
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Required Size:
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At least 3
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eigenVector3
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Description:
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A 3 element array containing the third component Eigenvector.
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Required Size:
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At least 3
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Syntax
mySpacecraftCovariance1.MapErrorEllipsoid(myArray1, myArray2, myArray3, myArray4);
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See also
SpacecraftCovariance Object
SpacecraftCovariance.MapErrorEllipsoid
Orbit Determination Guide
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