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1995-05-02
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Magellan Status 4/17/91
MAGELLAN STATUS REPORT
April 17, 1991
The Magellan spacecraft and its radar system are performing
well. Five star calibrations Tuesday were fully successful, with
two partially successful. The attitude updates still average
less than .02 degree. The spacecraft is now performing momentum
wheel desaturations on every other orbit and star calibrations
every orbit.
The weekly command sequence was successfully set to
Magellan late Tuesday and is now being executed. This new mapping
sequence includes two eight-minute "hide" periods in each three
hour and 15-minute orbit. During that period the spacecraft is
shaded by the high-gain antenna for thermal control. The maneuver
is necessary because the geometry of the planets in relation to
the sun places the spacecraft in direct sunlight for too long a
period of time.
As of this report, there has only been one orbit with the
hide sequences and there appears to be a cooling trend.
The hide periods will increase from now through the end of
the primary mission May 15. Next week, for example, there will be
two 12-minute hide periods in each orbit which will cut the 37.2-
minute mapping swath by 4.5 minutes.
In the following weeks, the hide periods increase to 23
minutes, which will cut mapping by 10 minutes, and then 36
minutes of hide period which will cut mapping by 15 minutes.
_____
AJS
4-17-91
9:00 AM
MAGELLAN STATUS REPORT
1. The Magellan spacecraft and its radar system are
performing nominally.
2. Five the STARCALS yesterday were fully successful, with
two partially successful. The attitude updates still
average less than .02 degree. The spacecraft is now
performing DESATS on every other orbit and STARCALS every
orbit.
3. The weekly command sequence M1107 was successfully sent
to Magellan along with the radar control parameter and
mapping quaternion files, and is now executing. As of
this report time, we have seen only one orbit of the "Two-
Hide" sequence, and there appears to be a definite cooling
trend.
___________________
AJS (pca)
4/17/91
MAGELLAN SPECIAL REPORT
SCIENCE DATA PRODUCTS
During the primary mission, the Project has frequently
reported on the number of mapping orbits completed and the
orbits for which data was successfully transmitted to the
earth. The ultimate measure of mission success, however, is
the production and distribution of final scientific data
products.
End-to-End Data Flow
The flow of data from the radar sensor onto the spacecraft
tape recorder, its transmission to Earth where it is again
recorded on tape as Original Data Records (ODRs), the
conversion of ODRs to Experiment Data Records (EDRs), then
into Full-Resolution Basic Image Data Records (F-BIDR's) and
various mosaics (F-MIDRs, C1-MIDRs, etc) is one of the major
challenges of the Magellan mission.
1. The radar sensor transmits bursts of radar pulses toward
the surface of Venus. A portion of each radar echo is
quantized to generate 16-bit data samples at a rate pf
2.26 x 106 samples per second. These are compressed by
the Block Adaptive Quantizer to reduce the bits-per-sample
from 16 to 4. The data acquired during each burst of
pulses is stored in a buffer memory and then sent to the
spacecraft tape recorder at a uniform rate of 800 kbps for
each 37.2 minute mapping pass. Thus, Magellan produces
1.8 x 109 bits per orbit.
2. The spacecraft tape recorder is played back at a 268.8
kbps rate and transmitted via an X-band communication link
to the Deep Space Tracking stations, where the data is
recorded on standard computer-compatible, 3/4 inch
magnetic tapes at a recording density of 6,250 bytes/inch.
The data from each orbit normally requires two 2400 foot
reels of tape. These tapes are called Original Data
Records (ODRs).
3. During the first mission cycle, the ODRs from Goldstone
are driven into JPL daily. ODRs at the Madrid and
Canberra stations are collected for one week then flown to
JPL. Although these ODRs can take as much as 21 days to
reach JPL, the current backlog is about 12 days.
4. Processing of data tapes is coordinated by Magellan's Data
Management and Archive Team (DMAT) which schedules each
stage of data processing from ODRs to EDRs to various
image products. DMAT also catalogs and stores the data
tapes.
5. ODR tapes are logged by DMAT and delivered to the Magellan
High Rate (MHR) processor where the station overlap is
removed, and ancillary data needed for further processing
and user information is added to produce the Experiment
Data Records (EDRs).
6. EDRs are then logged by DMAT and forwarded to the SAR Data
Processing Subsystem (SDPS) in Building 300. SDPS
operates on a two eight hour shift basis, Monday through
Friday. Here the 1.8 x 109 bits per orbit of raw radar
data from each SARvEDR is converted into 0.8 x 109 bits of
image data for each orbit and combined with ancillary data
to form Full Resolution Basic Image Data Record tapes (F-
BIDRs). F-BIDRs contain the long thin strips of orbit
image data which cover an area on Venus approximately 12
miles wide and 10,000 miles long (20 by 17,000 KM).
Understandably, these are called "radar noodles".
7. As a check of the data quality and interpretability, the
F-BIDRs are also delivered as long thermal prints to the
science work area. On each print the "noodle" is
presented in four parallel pieces approximately 1 inch
wide by 15 feet long.
8. The F-BIDRs are transmitted electronically to the Image
Data Processing Subsystem, (IDPS) in Building 168 to
connect the digital form of these thin image strips into
Mosaicked Image Data Record (MIDR) products:
a. F-MIDRs: The highest resolution image mosaics are the
Full-resolution MIDRs. These are images of 300 x 340 mile
(500 x 532 KM) areas of the Venus surface with a pixel
spacing of 75 meters. F-MIDRs will be produced for about
15% of the total surface area.
b. C1-MIDRs: These mosaicked products compress the full
resolution pixel data by averaging each 3 x 3 array into a
single pixel value. Each frame covers an area on Venus
measuring approximately 900 x 1000 miles (1450 x 1600 KM).
c. C2 & C3-MIDRs: These products further compress the
pixel arrays by averaging 9 x 9 and 27 x 27 arrays of full
resolution data. The C2 frames cover 45 degrees of
latitude, and 45 to 72 degrees of longitude. The C3
frames cover 80 degrees of latitude by 120 degrees of
longitude. All of the surface of Venus can be displayed
in six C3MIDRs.
d. PIDRs: These are Polar Image Data Records, specifically
designed for the polar areas of the planet. They contain
portions of adjacent F-BIDRs covering the area from 80x
latitude to the North Pole.
9. In addition to the image data record products, altimetry
and radiometry data products are being produced by
investigators at the Massachusetts Institute of
Technology. These include:
a. ARCDRs - Altimeter/Radiometer Composite Data Records
b. GTDRs - Global Topographic Data Records
c. GSDRs - Global Slope Data Records
d. GEDRs - Global Emissivity Data Records
e. GREDRs - Global Reflectivity Data Records
10. CD-ROMs: Many science data products end up as images,
either printed as photos or distributed as digital
records. Many of the science investigators need the
digital records because there are many analysis tools
which can be applied to this computer-readable form of the
images. It is the Project's plan to distribute the images
to the science community in the form of
CD-ROM = Compact Disk - Read Only Memory compact disks (CD-
ROMs). The first of these CD-ROMs was made available
on March 8, 1991, and contained ten full resolution
mosaicks from the first 24 orbits, i.e. the first 3
days of mapping.
The second CD-ROM includes mosaicks from the first 21 days
of mapping is scheduled for release to the science
community on April 19, 1991.
The third CD-ROM, containing full resolution mosaicks
beyond the first 21 days, is being used to test the
production system for CD-ROMs and will not be distributed
until about mid-summer. Work is proceeding, however, on
CD-ROMs 4, 5 and 6, containing images from the first 21
days of mapping. The goal is to release these about May
17. The Project is preparing for the production of 50-60
CD-ROMs in the remainder of calendar 1991, including
images from all of Cycle 1, on a schedule of about two per
week.
CD-ROMs will also be used to distribute these other
science data records. The first Altimeter/Radiometer
Composite Data Record disk is scheduled for production,
starting in late April, with release to the science
community in June.
11. Perhaps the most striking visual form of the data are the
simulated flights over the surface of Venus produced frame
by frame by combining the Magellan image and altimeter
data. Videos of 2,000 to 5,000 mile flights over and
around significant surface features will be produced every
three months. (This process is itself a unique story and
will be described in a future special report.)
Development of the Magellan Data Processing System
Due to budget constraints, the completion of Magellan
processing system was deferred until after launch. Throughout
cruise, final software development and test and system
integration and test were accomplished, targeted for
completion by May 1990. This represented a major development
challenge in addition to operating the Spacecraft. While most
of the system was in place by May 1991, certain software
builds took most of the summer to complete, but were ready for
mapping operations prior to arrival at Venus.
The Magellan processing challenge for a planetary mission is
unique and quite large. The Magellan system is required to
process one week of acquired data in one week --- the highest
rate and the longest duration for any planetary mission.
Previous planetary encounters consisted of intense near
encounter phases lasting for a few months, over which large
volumes of data are collected, followed by many months of
quieter cruise activities.
Magellan's "Near Encounter"
Magellan continues in an intensive "near encounter" phase for
243 days, the time it takes the planet to rotate once
underneath the spacecraft. During this time, data are
collected on each 3.25 hour orbit, 24 hours a day, 7 days a
week. In seven months Magellan collected more data bits than
all the Mariners, Vikings and Voyagers. At the end of the
primary mission, the "near encounter" continues into the next
243-day cycle, then the next and the next.
At the start of mapping on 15 September, the data processing
system began to immediately produce high quality data
products. The first three weeks of radar data processing
operations concentrated on engineering refinements,
performance tests, and special product generation to support
initial press conferences. The standard data processing
activity started on October 9th. Several refinements were
made to correct problems that have been discovered during
operations.
The malfunction of one of the spacecraft tape recorders
resulted in several modifications to data processing to
alleviate the effects of the resulting damage in the received
radar data. The recent experience indicates that the planned
Cycle 1 data products will all be completed by the original
schedule date of June 28, 1991.
SPACELINK NOTE: For information on obtaining the CD-ROM disk, contact:
National Space Science Data Center
NASA/Goddard Space Flight Center
Code 633
Greenbelt, MD 20771
301/286-6695