DATA_SET_DESCRIPTION |
Data Set Overview
=================
The Giotto Radio Science Original Experiment Data Set was
generated by ground equipment connected to the Canberra 64-m
antenna of the NASA Deep Space Network (DSN) in Australia. It
includes two types of data -- an Archival Tracking Data File
(ATDF) from closed loop receivers and Original Data Records
(ODRs) from open loop receivers. These should be considered
'raw' data which much be processed before being applied to
science problems. The data in 'GIO-C-GRE-3-RDR-HALLEY-V1.0' have
been partially processed and may be more suitable for immediate
science application.
ATDFs are files of radiometric data produced by the Network
Operations Control Center (NOCC) Navigation Subsystem (NAV). They
are derived from Intermediate Data Records by NAV and contain all
radiometric measurements received from the DSN station including
signal levels, antenna pointing angles, Doppler, range, and
residuals. Doppler data are often used to infer spacecraft
radial motion relative to the tracking antenna -- in this case to
determine the reduction in velocity when Giotto passed through
the dust and gas surrounding Comet Halley. Data values in ATDFs
are reported at rates no higher than 10 per second.
One ATDF is included in this data set. It covers the time
interval 1986-03-13T15:32:47 to 1986-03-14T05:10:00.
ODRs are files of digitally sampled medium-bandwidth receiver
output. In conjunction with gain settings and receiver tuning
information (contained in the ODR header) these files allow the
investigator to derive the amplitude and frequency of the Giotto
radio signal to highest accuracy with post-experiment processing.
For the Giotto Radio Experiment an open-loop receiver bandwidth
of 25 kHz was selected, and 8-bit sampling was performed on each
of four channels. The channel assignments were: (1) S-RCP, (2)
S-LCP, (3) X-RCP, and (4) X-LCP where S-Band signals are at 13 cm
wavelength, X-Band signals are at 3.6 cm wavelength, RCP denotes
right circular polarization, and LCP denotes left circular
polarization. During the Giotto experiment only X-RCP was
transmitted by the spacecraft, so channels (1) and (2) should
contain only noise and channel (4) should contain, at most, a
leakage signal.
Two ODR files are included in this data set; each covers eight
minutes. Together they cover the Giotto Halley encounter. Their
start times (UTC) are 1986-03-13T23:56:02 and 1986-03-14T00:04:02
The measurements of frequency and frequency residual may be
converted to changes in spacecraft velocity during the Halley
encounter. The changes in velocity may then be interpreted in
terms of mass fluence (dust and gas) within Halley's coma
[EDENHOFERETAL1986A], [EDENHOFERETAL1986B], [EDENHOFERETAL1986C],
[EDENHOFERETAL1986D], [EDENHOFERETAL1987A].
More detailed analyses of the dynamics of the spacecraft as
inferred from the GRE data have been published by [BIRDETAL1988],
[PAETZOLDETAL1988], [PAETZOLDETAL1990], [PAETZOLDETAL1991A],
[PAETZOLDETAL1991B], and [PAETZOLDETAL1991C].
Parameters
==========
Each ATDF data record contains 117 parameters. These include
estimates of received signal strength and frequency as well as
status information on components of the DSN system. The ATDF is
described by a Software Interface Specification, included as
TRK_2_25.TXT in the DOCUMENT directory of the data set archival
volume. A complete list of parameters is given in Table 3 of
that document.
Open loop data records contain 8-bit samples of receiver output
as described above. Each block of 4000 data samples is
accompanied an 80 byte header, a 300 byte trailer of Precision
Power Monitor data, and a 10 byte trailer of operator-entered
timing and frequency offsets. The ODR is described by a Software
Interface Specification, included as RSC_11_9.TXT in the DOCUMENT
directory of the data set archival volume. A complete list of
header parameters is given in Figure RSC-11-9-1 in that document.
Processing
==========
DSN NAV performs editing on data during conversion from the IDR
to ATDF formats; this function serves mostly to remove anomalous
(out of nominal range) values.
Open loop data are not edited or otherwise processed.
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CONFIDENCE_LEVEL_NOTE |
[EDENHOFERETAL1987B] reported that
'The maximum frequency offset in the one-way data was 16.9 Hz.
But the two-way data acquired before and after the encounter are
consistent with a maximum of only 4.64 Hz.'
Two explanations have been offered [EDENHOFERETAL1987B]. First is
that the drag forces amplified the oscillator drift through
acoustic, electrical, or thermal energy deposition. In this
case, the measurements differ from the actual values by only a
scale factor. The analysis presented by [EDENHOFERETAL1987B]
adopts this assumption.
The second explanation is that transients during the encounter
(possibly associated with failure of the NMS experiment and
switching of the TWT amplifier tubes) also induced a frequency
offset in the on-board oscillator. In this case, both an offset
and a scale factor may be needed to correct the data.
No applicable pre-launch tests were conducted on the radio system
to allow choosing between these assumptions.
There is no other information on quality of the data. It is
believe that operations during data acquisition were nominal and
that these two data types represent the highest quality raw data
that could be obtained under the circumstances.
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