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comet
Function
The comet shell command puts Argo Navis
processing state. When the comet command is issued, Argo Navis
'OK'
Orbital element files can be
same orbital element format as TheSky
22P/Kopff
86P/Wild 3
129P/Shoemaker-Levy 3
C/2002 C1 (Ikeya-Zhang)
C/2002 C2 (LINEAR)
P/2002 CW134 (LINEAR)
C/2002 E2 (Snyder-Murakami)
C/2002 F1 (Utsunomiya)
C/2002 H2 (LINEAR)
C/2002 J4 (NEAT)
While in the comet orbital element processing state, Argo Navis
line at a time. A line can either be –
•
An empty line, or
•
An orbital element entry as above, or
•
A comet state command
All state commands begin with a '#' character. These state commands are as follows –
•
#Quit : Leave the comet state and return to the shell
•
#Write : Commit all loadable catalog data to FLASH
•
#Count : Return a count of how many comet elements are currently loaded.
•
#Purge : Remove the comet catalog from RAM
•
#Memory : Report free space in bytes in loadable catalog memory pool
•
#Delete <OBJECT> : Delete the specified comet from RAM
All input lines, except #Count, #Memory and #Quit commands, will be responded to with
either –
•
OK
•
ERROR: <MESSAGE>
Argo Navis
User Manual Edition 11, Dec 2014, for
Argo Navis™
downloaded
from the Internet. Argo Navis
software package. An example file follows –
TM
|2000|20021212.0944 | 1.583616 |0.543212 |162.7603 |120.9293 |
|2000|20010618.4822 | 2.309902 |0.364447 |179.1225 | 72.6090 | 15.4380 |11.0 |15.0 | MPC 3166
|2000|20050603.7287 | 2.810134 |0.249392 |181.4039 |303.6526 |
|2000|20020318.9811 | 0.507053 |0.990129 | 34.6669 | 93.3696 | 28.1218 | 7.0 |10.0 | MPEC 2002-H23
|2000|20020410.7764 | 3.253938 |1.000000 |159.9244 |242.9541 |104.8846 | 8.5 |10.0 | MPEC 2002-F22
|2000|20020228.9470 | 1.839612 |0.489434 |190.1120 |348.3179 | 15.2273 |13.0 |10.0 | MPEC 2002-G39
|2000|20020221.7737 | 1.466270 |1.000115 |
|2000|20020422.8984 | 0.438299 |0.999556 |125.8999 |289.0295 | 80.8765 | 8.5 |10.0 | MPEC 2002-J10
|2000|20020323.5875 | 1.636079 |1.000000 | 20.5431 |269.0400 |110.5088 |10.5 |10.0 | MPEC 2002-J36
|2000|20031001.301
| 3.62793
|1.00000
Argo Navis™
into the comet orbital element
TM
4.7185 | 3.0 |26.0 | MPC 34423
5.0120 |11.0 |10.0 | MPC 30739
9.0185 |244.5781 | 92.5440 | 7.5 |10.0 | MPEC 2002-J35
|230.588
| 70.992
| 46.333
™
Model 102/102B, Firmware Vers.3.0.0
will respond with
TM
uses the
TM
| 5.5 |10.0 | MPEC 2002-J47
processes input a
TM
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