SpacecraftCovariance.GetStateSigmasInFrame Method

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Description

Returns an array containing the square root of the diagonal elements 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.

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Overload List

Signatures

Return Value

Description

SpacecraftCovariance.GetStateSigmasInFrame(CoordinateSystem coordinate_system)

Array

Returns an array containing the square root of the diagonal elements of the spacecraft state in the specified attitude reference frame. This method is only used with the Cartesian element set.

SpacecraftCovariance.GetStateSigmasInFrame(String referenceFrame)

Array

Returns an array containing the square root of the diagonal elements of the spacecraft state in the specified attitude reference frame. This method is only used with the Cartesian element set.

 

 

See also

SpacecraftCovariance Object

Orbit Determination Guide