CoordinateSystem ================ .. py:class:: ansys.stk.core.stkutil.CoordinateSystem IntEnum .. py:currentmodule:: CoordinateSystem Overview -------- .. tab-set:: .. tab-item:: Members .. list-table:: :header-rows: 0 :widths: auto * - :py:attr:`~UNKNOWN` - Represents coordinate system not supported by the Object Model. * - :py:attr:`~ALIGNMENT_AT_EPOCH` - Alignment at Epoch: an inertial system coincident with ECF at the Coord Epoch. Often used to specify launch trajectories. * - :py:attr:`~B1950` - B1950: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the beginning of the Besselian year 1950 and corresponds to 31 December 1949 22:09:07.2 or JD 2433282.423. * - :py:attr:`~FIXED` - Fixed: X is fixed at 0 deg longitude, Y is fixed at 90 deg longitude, and Z is directed toward the north pole. * - :py:attr:`~J2000` - J2000: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth on 1 Jan 2000 at 12:00:00.00 TDB, which corresponds to JD 2451545.0 TDB. * - :py:attr:`~MEAN_OF_DATE` - Mean of Date: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the Orbit Epoch. * - :py:attr:`~MEAN_OF_EPOCH` - Mean of Epoch: X points toward the mean vernal equinox and Z points along the mean rotation axis of the Earth at the Coord Epoch. * - :py:attr:`~TEME_OF_DATE` - TEME of Date: X points toward the mean vernal equinox and Z points along the true rotation axis of the Earth at the Orbit Epoch. * - :py:attr:`~TEME_OF_EPOCH` - TEME of Epoch: X points toward the mean vernal equinox and Z points along the true rotation axis of the Earth at the Coord Epoch. * - :py:attr:`~TRUE_OF_DATE` - True of Date: X points toward the true vernal equinox and Z points along the true rotation axis of the Earth at the Orbit Epoch. * - :py:attr:`~TRUE_OF_EPOCH` - True of Epoch: X points toward the true vernal equinox and Z points along the true rotation axis of the Earth at the Coord Epoch. * - :py:attr:`~TRUE_OF_REFERENCE_DATE` - True of Ref Date: A special case of True of Epoch. Instead of the Coord Epoch, this system uses a Reference Date defined in the Integration Control page of the scenario's PODS properties. * - :py:attr:`~ICRF` - ICRF: International Celestial Reference Frame. * - :py:attr:`~MEAN_EARTH` - Mean Earth. * - :py:attr:`~FIXED_NO_LIBRATION` - uses an analytic formula not modeling lunar libration. * - :py:attr:`~FIXED_IAU2003` - Fixed_IAU2003. * - :py:attr:`~PRINCIPAL_AXES421` - PrincipalAxes_421. * - :py:attr:`~PRINCIPAL_AXES403` - PrincipalAxes_403. * - :py:attr:`~INERTIAL` - Inertial. * - :py:attr:`~J2000_ECLIPTIC` - The mean ecliptic system evaluated at the J2000 epoch. The mean ecliptic plane is defined as the rotation of the J2000 XY plane about the J2000 X axis by the mean obliquity defined using FK5 IAU76 theory. * - :py:attr:`~TRUE_ECLIPTIC_OF_DATE` - The true ecliptic system, evaluated at each given time. The true ecliptic plane is defined as the rotation of the J2000 XY plane about the J2000 X axis by the true obliquity defined using FK5 IAU76 theory. * - :py:attr:`~PRINCIPAL_AXES430` - PrincipalAxes_430. * - :py:attr:`~TRUE_OF_DATE_ROTATING` - TrueOfDateRotating: Like the Fixed system, but ignores pole wander. The XY plane is the same as the XY plane of the TrueOfDate system, and the system rotates about the TrueOfDate Z-axis. * - :py:attr:`~ECLIPTIC_J2000ICRF` - EclipticJ2000ICRF: An ecliptic system that is a fixed offset of the ICRF system, found by rotating the ICRF system about its X-axis by the mean obliquity at the J2000 epoch (i.e., 84381.448 arcSecs). The ecliptic plane is the XY-plane of this system. Import detail ------------- .. code-block:: python from ansys.stk.core.stkutil import CoordinateSystem