SpacecraftCovariance.SetCovarianceInFrame Method |
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DescriptionSets 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. Click here to see the documentation for this object in millisecond timing precision mode.
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