Scenario: CB Inertial To Fixed Quaternions: MeanOfDate

The mean equator mean equinox coordinate system evaluated at the requested time.

Name Dimension Type Description
Time DateFormat Real Number Time.
q1 Unitless Real Number First element of quaternion (and of its vector part) representing orientation between the two sets of axes.
q2 Unitless Real Number Second element of quaternion (and of its vector part) representing orientation between the two sets of axes.
q3 Unitless Real Number Third element of quaternion (and of its vector part) representing orientation between the two sets of axes.
q4 Unitless Real Number Fourth element of quaternion (its scalar part) representing orientation between the two sets of axes.

STK Programming Interface 11.0.1