SpacecraftCovariance.SetCovarianceInFrame Method

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Description

Sets the covariance of the spacecraft state in the inertial reference frame, after converting from 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.SetCovarianceInFrame(CoordinateSystem coordinate_system, Matrix inputCovarianceInFrame)	None	Sets the covariance of the spacecraft state in the inertial reference frame, after converting from the specified attitude reference frame. This method is only used with the Cartesian element set.
SpacecraftCovariance.SetCovarianceInFrame(String inputReferenceFrame, Matrix inputCovarianceInFrame)	None	Sets the covariance of the spacecraft state in the inertial reference frame, after converting from the specified attitude reference frame. This method is only used with the Cartesian element set.

See also

SpacecraftCovariance Object

Orbit Determination Guide