PropagatorRealtimePointBuilder#

class ansys.stk.core.stkobjects.PropagatorRealtimePointBuilder#: Allow the user to create vehicle’s ephemeris by appending ephemeris points.

Overview#

Methods

`get_points_in_frame`	Allow adding points using specified reference frame.
`remove_all_points`	Remove any points add to the vehicle’s realtime ephemeris.

Properties

`ephemeris_in_b1950_frame`	The input values are in the B1950 coordinate frame.
`ephemeris_in_central_body_fixed_frame`	Origin is at the center of the Earth and axes which are fixed to the Earth.
`ephemeris_in_central_body_inertial_frame`	Origin is at the center of the Earth and axes which are fixed in inertial space. The inertial coordinate system is J2000.
`ephemeris_in_heading_pitch`	Lat & Lon are entered in Lat & Lon units. Alt is in Distance unit. Heading & Pitch are in degrees. Speed is in Distance/Time. Heading is entered as degrees from North and is the rotation about the Z-axis; Pitch is the rotation about the Y-axis.
`ephemeris_in_latitude_longituide_altitude`	The LLA measures <Alt> from the surface of the Earth, or 0.
`ephemeris_in_latitude_longitude_altitude_above_terrain`	The AGL_LLA considers terrain at the specified location when measuring <Alt>.
`ephemeris_in_latitude_longitude_altitude_above_mean_sea_level_`	The MSL_LLA considers mean sea level at the specified location when measuring <Alt>.
`ephemeris_in_utm`	Valid values for ZoneStr are A, B, Y, Z or ddc, where 00<dd<61 and c is C-X. Easting, Northing and Alt are entered in distance units. LonRate and LatRate are entered in degrees/second. AltRate is entered in units/second.

from ansys.stk.core.stkobjects import PropagatorRealtimePointBuilder

property PropagatorRealtimePointBuilder.ephemeris_in_b1950_frame: PropagatorRealtimeCartesianPoints#: The input values are in the B1950 coordinate frame.

property PropagatorRealtimePointBuilder.ephemeris_in_central_body_fixed_frame: PropagatorRealtimeCartesianPoints#: Origin is at the center of the Earth and axes which are fixed to the Earth.

property PropagatorRealtimePointBuilder.ephemeris_in_central_body_inertial_frame: PropagatorRealtimeCartesianPoints#: Origin is at the center of the Earth and axes which are fixed in inertial space. The inertial coordinate system is J2000.

property PropagatorRealtimePointBuilder.ephemeris_in_heading_pitch: PropagatorRealtimeHeadingPitch#: Lat & Lon are entered in Lat & Lon units. Alt is in Distance unit. Heading & Pitch are in degrees. Speed is in Distance/Time. Heading is entered as degrees from North and is the rotation about the Z-axis; Pitch is the rotation about the Y-axis.

property PropagatorRealtimePointBuilder.ephemeris_in_latitude_longituide_altitude: PropagatorRealtimeDeticPoints#: The LLA measures <Alt> from the surface of the Earth, or 0.

property PropagatorRealtimePointBuilder.ephemeris_in_latitude_longitude_altitude_above_terrain: PropagatorRealtimeDeticPoints#: The AGL_LLA considers terrain at the specified location when measuring <Alt>.

property PropagatorRealtimePointBuilder.ephemeris_in_latitude_longitude_altitude_above_mean_sea_level_: PropagatorRealtimeDeticPoints#: The MSL_LLA considers mean sea level at the specified location when measuring <Alt>.

property PropagatorRealtimePointBuilder.ephemeris_in_utm: PropagatorRealtimeUTMPoints#: Valid values for ZoneStr are A, B, Y, Z or ddc, where 00<dd<61 and c is C-X. Easting, Northing and Alt are entered in distance units. LonRate and LatRate are entered in degrees/second. AltRate is entered in units/second.

PropagatorRealtimePointBuilder.get_points_in_frame(self, reference_frame: str) → PropagatorRealtimeCartesianPoints#

Allow adding points using specified reference frame.

PropagatorRealtimePointBuilder.remove_all_points(self) → None#

Remove any points add to the vehicle’s realtime ephemeris.