Aircraft: Cartesian Acceleration: J2000
The mean equator mean equinox coordinate
system evaluated at the J2000.0 epoch (2000 January 1.5 = JD
2451545.0 TDB).
| Name |
Dimension |
Type |
Description |
| Time |
DateFormat |
Real Number |
Time. |
| x |
Acceleration |
Real Number |
The X component of the acceleration vector. |
| y |
Acceleration |
Real Number |
The Y component of the acceleration vector. |
| z |
Acceleration |
Real Number |
The Z component of the acceleration vector. |
| magnitude |
Acceleration |
Real Number |
The non-rotating coordinate system coincident with
the Fixed system evaluated at the object's coordinate reference
epoch. |
STK Programming Interface 11.0.1