DATA_SET_DESCRIPTION |
Data Set Overview
=================
This data set consists of magnetic field vector data recorded
by the Fluxgate Magnetometer onboard the Pioneer 11 spacecraft,
during the Jupiter encounter period. Data include 5 minute
averages of the magnetic field in both Inertial Heliocentric
and System III (1957.0) coordinates. Spacecraft trajectory
data are also provided, in System I and System III (1957.0)
coordinates.
Data Sampling
==============
The fluxgate magnetometer data is multiplexed into one of
the Science Subcom formats available on the spacecraft.
Two separate 6-bit words per subcom cycle are assigned
to the instrument and thus 3 complete cycles are required
to read out the contents of the output buff. At a bit rate
of 2048 bps, a complete subcom cycle requires 6 second and
a vector measurement is obtained approximately every 18 to
24 second depending on the actual roll rate of the spacecraft,
which is nominally 5 revolutions per minute (ACUNA&NESS1974).
The NSSDC documentation does not contain information about what
data resolution this data set (5 minute) is averaged from.
Data Processing
===============
No detailed information of data processing is found in the NSSDC
documentation pertinent to this data set.
Pioneer 11 spacecraft was operating under a spin-stablized
condition and had a spin period of 12 seconds.
Data Format
============
The Pioneer 11 magnetometer data for Jupiter encounter were
originally written on a BCD magnetic tape created at NSSDC from
a card deck supplied by the PI team. The original file was
re-formatted into a new ASCII file named P11_FGM_JUP_ENC_5MIN.TAB
which contains the following data columns:
--------------------------------------------------------------------
Column Column Column
Name Format Description
--------------------------------------------------------------------
TIME A24 Ground received time in yyyy-mm-ddThh:mm:ss.sssZ
R F5.2 Distance of Pioneer 11 from Jupiter in Rj
LAT F6.1 Latitude of Pioneer 11 in System III (1957.0)
LON1 F7.1 Longitude of Pioneer 11 in System I
LON3 F7.1 Longitude of Pioneer 11 in System III (1957.0)
BX F8.4 X component of the magnetic field in Inertial
Heliocentric coordinates
BY F8.4 Y component of the magnetic field in Inertial
Heliocentric coordinates
Bz F8.4 Z component of the magnetic field in Inertial
Heliocentric coordinates
BR F8.4 Radial component of the magnetic field in
System III (1957.0)
BTHETA F8.4 Polar component of the magnetic field in
System III (1957.0)
BPHI F8.4 Azimuthal component of the magnetic field in
System III (1957.0)
N I2 Number of data points used in averaging
--------------------------------------------------------------------
Coordinate System for Data
===========================
System I is a planetographic spherical coordinates at Jupiter. This
system used a relatively faster Jupiter spin rate (877.90 degree per
24 hours) to describe cloud features within 10 degree of the equator.
The Central Meridian Longitude was established at 12:00 Greenwich Mean
Time on July 14, 1897.
System III (1957.0) is a planetographic spherical coordinates. In this
system, the Jovian rotation period is defined to be 9h55m29.37s
and the Central Meridian Longitude is defined at 00:00 UT on
January 1, 1957.
Inertial Heliocentric coordinates is a Cartesian system, defined based
on two principle directions, the Jupiter spin axis J, and the direction
from the sun to the first point of Aries, X. The Y direction is given
by the cross product of J and X. The Z direction is defined as the
cross product of X and Y.
Ancillary Data
==============
There is no ancillary data associated with this data set.
Instrument Calibration
======================
The fluxgate magnetometer was calibrated at the GSFC Magnetic
Test Facility by means of a 2 meter diameter, single axis
Helmholtz coil system. Typically hysteresis observed after
exposure to 2.5 mT fields was less than 1 part in 10**3 (one
count). Temperature stability is better than +- 0.5% over the
temperature range of -20 to +40 degree Celsius in spite of the
open loop design of the instrument. This is due to the fact
that the characteristics of the magnetic material used in the
sensor cores are fairly independent of temperature over the
indicated range. The stability figure includes the A/D converter
drift and a large portion of it is due to the single ramp design
of the latter. Nevertheless, minimum power consumption
requirements and flight qualified component availability
precluded the used of more stable A/D converter designs
(ACUNA&NESS1974).
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