ORBIT_DETERMINATION_UPDATED¶
event_output for ORBIT_DETERMINATION_UPDATED.
Format¶
<time> ORBIT_DETERMINATION_UPDATED {target name | "(" track id ")"} " TrackId: " <track id>
Orbital Elements: SMA: <length> ECC: <angle> INC: <angle> RAAN: <angle> ARGP: <angle> MA: <angle> TA: <angle>
Breakdown¶
- <time>
The current simulation time
- <platform>
The name of the platform initiating the maneuver.
- {target name | “(” track id “)”}
The truth target name if available; otherwise the track id.
- <track id>
The local track id upon which orbit determination is being performed.
- Orbital Elements: The current orbital elements of the determined orbit.
- SMA: <length>
Semi-major axis (km)
- ECC: <double>
Eccentricity
- INC: <angle>
Inclination (degrees)
- RAAN: <angle>
Right ascension of the ascending node (degrees)
- ARGP: <angle>
Argument of periapsis (degrees)
- MA: <angle>
Mean anomaly (degrees)
- TA: <angle>
True anomaly (degrees)
How it Appears in Output¶
7063.66267 ORBIT_DETERMINATION_UPDATED commander RADIO_ROSTO_(RS-15)(23439) \
Orbital Elements: SMA: 8223.421525 km ECC: 0.03657859452 INC: 64.80713641 deg RAAN: 330.8742166 deg ARGP: 279.2482824 deg MA: 172.0386202 deg TA: 172.5939801 deg
How to Show Event Messages¶
event_output file replay.evt # write event messages to file "replay.evt" enable ORBIT_DETERMINATION_UPDATED end_event_output
