SpacecraftCovariance.MapErrorEllipsoid 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 nanosecond timing precision mode.

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

 

Overload List

Signatures

Return Value

Description

SpacecraftCovariance.MapErrorEllipsoid(Array eigenValues, CoordinateSystem dcm)

None

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

SpacecraftCovariance.MapErrorEllipsoid(ProximityZone zone, Variable kSigmaValue)

None

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

SpacecraftCovariance.MapErrorEllipsoid(Array eigenValues, Array eigenVector1, Array eigenVector2, Array eigenVector3)

None

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

 

 

See also

SpacecraftCovariance Object

Orbit Determination Guide