ORBIT_DETERMINATION_INITIATED¶
event_output for ORBIT_DETERMINATION_INITIATED.
Format¶
<time> ORBIT_DETERMINATION_INITIATED {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¶
463.66267 ORBIT_DETERMINATION_INITIATED commander RADIO_ROSTO_(RS-15)(23439) \
Orbital Elements: SMA: 8399.093606 km ECC: 0.01611561155 INC: 64.81879666 deg RAAN: 330.9362248 deg ARGP: 297.6253149 deg MA: 203.3773086 deg TA: 202.6578931 deg
How to Show Event Messages¶
event_output file replay.evt # write event messages to file "replay.evt" enable ORBIT_DETERMINATION_INITIATED end_event_output
