| Name: Vector_Cartesian_Position_Central_Body_To_Spacecraft | Version Id: 1.0.0.0 | ||
|---|---|---|---|
| Description:The Vector_Cartesian_Position_Central_Body_To_Spacecraft is a linear, rectangular coordinates vector from the center of mass of the central body (e.g., planet) to the spacecraft. While the class Coordinate_System_Identification is optional, it must be used here if the coordinate system has not been specified in the enclosing class. | |||
| Namespace Id: geom | Steward: geo | Role: TBD_role | Status: Active |
| Class Hierarchy: Vector_Cartesian_Position_Base :: Vector_Cartesian_Position_Extended_Base :: Vector_Cartesian_Position_Central_Body_To_Spacecraft | |||
| Attribute(s) | Name | Cardinality | Value |
| x_position | 1..1 | None | |
| y_position | 1..1 | None | |
| z_position | 1..1 | None | |
| light_time_correction_applied | 1..1 | None, Received_Light_Time, Received_Light_Time_Stellar_Abb, Transmitted_Light_Time, Transmitted_Light_Time_Stellar_Abb | |
| Association(s) | Name | Cardinality | Class |
| Coordinate_System_Identification | 0..1 | Coordinate_System_Identification | |
| Referenced from: Vectors_Cartesian_Specific | |||