AdvCAT: Secondary Vehicles

Lists values set for various parameters of each secondary object. This report is only valid after the AdvCAT computation has been performed.

Type: Fixed data. Intended to be used only with elements from this same data provider.

Availability: Reports

Name Dimension Type Description
Epoch DateFormat Real Number The reference epoch for the object.
Normal DistanceUnit Real Number or Text If the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the normal direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
Status Unitless Text An error status indicator.
StringID Unitless Text The string identifier of the secondary object involved in the close approach event. If the object has no string identifier, then the value will be "Not Avail".
Cross-Track DistanceUnit Real Number or Text If the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the cross-track direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
HardBodyRadius SmallDistanceUnit Real Number The hard body radius value used for this object.
Source Unitless Text Planetary Ephemeris data file type (i.e. JPL) and the actual files (i.e. DE430/LE430).
Type Unitless Text The type of primary object.
Name Unitless Text Object name that experienced an error.
Tangential DistanceUnit Real Number or Text If the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the tangential direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
NumberID Unitless Text The number identifier of the secondary object involved in the close approach event. If the object has no number identifier, then the value will be "Not Avail".
SourceID Unitless Text The identifier of the object as used by the ephemeris source for the object. For example, the identifier for objects that use a GPS sem or yuma file is PRN-##.
SSC Unitless Text SSC number of the satellite with out of date TLE data for the date selected.
Start Time DateFormat Real Number The start time of an interval.
Stop Time DateFormat Real Number The stop time of an interval.

STK Programming Interface 11.0.1