DATASET_DESCRIPTION |
Data Set Overview
=================
Data Set Description
--------------------
This data set consists of Voyager 2 Saturn encounter ephemeris data
in Kronographic (L1) coordinates covering the period 1981-08-23 to
1981-08-29. Two versions, both covering the same time period, but
containing slightly different data, are provided. One version was
generated by the Voyager MAG team from Voyager 2 SEDR, the other
by the PDS/PPI node using the VG1_SAT.TSP and PCK00006.TPC SPICE
kernels.
Due to inaccuracies in Voyager SEDR, as well as changes in the
values of some key parameters (e.g. Saturnian radius) the timing
is improved for the SPICE generated data. However, since much
of the original analysis was based upon the SEDR generated
ephemeris, this data has been included as well.
SEDR generated ephemeris
------------------------
Instrument P.I. : N/A
Data Supplier : NSSDC
Data sampling rate : 96 seconds
Data Set Start Time : 1981-08-23T10:34:23.645Z
Data Set Stop Time : 1981-08-29T23:57:35.078Z
SPICE generated ephemeris
-------------------------
Instrument P.I. : N/A
Data Supplier : S. Joy
Data sampling rate : 96 seconds
Data Set Start Time : 1981-08-23T10:34:23.645Z
Data Set Stop Time : 1981-08-29T23:57:35.078Z
Parameters
==========
SEDR generated ephemeris
------------------------
PARAMETER RESOLUTION/ DESCRIPTION
NAME UNITS
time 96.0 Sec time of the sample (UT) in the format
yyyy-mm-ddThh:mm:ss.sssZ
m65536 counts spacecraft clock counts
mod60 counts
fds_line counts
sc_x R[J] kronocentric (L1) cartesian
sc_y R[J] cartesian position vectors: X, Y, and
sc_z R[J] Z
vel_x km/s kronocentric (L1) X, Y, and Z spacecraft
vel_y km/s velocity components
vel_z km/s
sc_r R[J] kronocentric (L1) spherical
sc_lat degrees coordinates position vectors: range,
sc_lon degrees latitude, and longitude
CartSys3_to_SphSys3 cartesian L1 coordinates to spherical L1
coordinates rotation matrix containing
9 1pe15.8 elements
SC_to_CartSys3 payload (spacecraft) to cartesian L1
coordinates rotation matrix containing
9 1pe15.8 elements
SC_to_SphSys3 payload (spacecraft) to spherical L1
coordinates rotation matrix containing
9 1pe15.8 elements
SPICE generated ephemeris
-------------------------
PARAMETER RESOLUTION/ DESCRIPTION
NAME UNITS
time 96.0 Sec time of the sample (UT) in the
format yyyy-mm-ddThh:mm:ss.sssZ
R AU kronocentric (L1) spherical coordinates
LAT degrees range, latitude, and longitude position
LON degrees
LocTime hours angular separation between the
meridian containing the sun and the
one containing the spacecraft
converted to a time. The sun meridian
is defined to be noon (12.000), with
midnight (0.000) opposite it. Dawn
(6.000) and dusk (18.000) are where
the sun rises and sets according to
the planet's rotation
Coordinate System
=================
The Kronographic (L1) coordinates is a Saturn centered spherical
system, based on the Saturn Longitude System (Voyager Measurements
of the Rotation Period of Saturn's Magnetic Field, Desch and Kaiser,
JGR, 8, 253, 1981). In this coordinate syatem, longitude increases
with time as viewed by a stationary remote observer.
In cartesian coordinates:
X points along the Saturn-Sun line in the solar
equatorial plane (positive towards the Sun)
Y completes the right handed set
Z points along the Saturn's spin axis, positive
In spherical coordinates:
R Saturn to spacecraft range (positive away from
Saturn)
LAT completes the left handed, orthogonal set
LON east longitude (with longitude increasing eastward
from a specific Saturnian prime meridian)
SPICE ephemeris were generated using the current definition of
the Saturnian radius, 60268 km. The spin rate used in generating
these data is the same as that used for System III (1965),
+870.536 degrees/24 hours.
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