Instructions to use K-4 VLBI system with FS9 software
Yasuhiro Koyama1(koyama(AT)nict.go.jp) and
William E. Himwich2
1 Kashima Space Research Center
Communications Research Laboratory
893-1 Hirai, Kashima, Ibaraki 314-0012, Japan
2Code 926.9, NVI Inc.,
Goddard Space Flight Center
National Aeronautics and Space Administration
Greenbelt, Maryland, 20771-0001 USA
1. Introduction
The K-4 VLBI data acquisition system has been developed by
Communications Research Laboratory and are currently used at
several VLBI stations. The system can be used for various
modes of geodetic and astronomical VLBI observations. Recently,
NASA Field System software has been implemented to be able to
control the K-4 system. In this document, characteristics and
specifications of the K-4 VLBI system are briefly described
and instructions to use Field System to control the K-4 VLBI
system are presented.
2. K-4 VLBI System
The K-4 VLBI data acquisition system at an observation station
consists of the units listed below. In addition to these units,
there are output interface units and correlator systems necessary
at the time of correlation processing, but these systems are not
supported by the Field System software and will not be described here.
Local Oscillator ..... 7632A, 7624
Video Converter ..... 7631A, 7623
Input Interface ..... DFC1100, DFC2100
Data Recorder ..... DIR1000, DIR1000L, DIR1000M
Tape Changer (Optional) ..... DMS24
The local oscillator unit generates phase locked local frequency
signals based on a reference 10MHz (or 5MHz) signal. These signals
are provided to the video converter unit where the IF signal is
down-converted to video band signals by using image rejection
mixers and low-pass filters. The model 7632A is capable to generate
16 local frequency signals from 99.9 MHz through 519.99 MHz,
whereas the model 7624 is capable to generate 8 local frequency
signals from 499.99 MHz through 999.99 MHz. The model 7631A
video converter can convert 16 video channels and is used with
the 7632A local oscillator unit. The model 7623 video converter can
convert 8 video channels and is used with the 7624 local oscillator
unit. In this case, two sets of each unit are used to configure 16
observation channels for usual geodetic VLBI experiments.
Both video converter units have multiple low pass filters
and the selectable bandwidths depend on the actual configuration
of the unit.
Input interface unit digitizes the video band signals and record
these signals by controlling the data recorder unit. DFC1100 has a
single observation mode of 1 bit sampling - 16 channel - 4 Mbps
(64 Mbps total). All three models of the data recorder unit can be
used with the DFC1100 input interface unit. On the other hand,
DFC2100 can be used with multiple observation modes. Among of these
modes, only three observation modes, i.e. 1) 1bit-16ch.-4Mbps,
2) 1bit-16ch.-8Mbps, and 3) 1bit-16ch.-16Mbps, are currently
supported by correlators at Koganei (CRL) and Tsukuba (GSI)
correlators, and are supported by FS9 software. The difference of
the three models of data recorder unit is the maximum speed of the
data recording. The maximum recording speed of model DIR1000 is
256 Mbps and all three observation modes are possible. On the
other hand, the maximum recording speeds of DIR1000L and DIR1000M
are 128 Mbps and 64 Mbps, respectively.
Tape changer unit can change 24 ID1 cassette tapes for un-attended
continuous observations. The current version of the FS9 software
does not support the unit yet. The implementation is under progress.
3. Setup
First, the /usr2/control/equip.ctl file should be edited to
reflect the actual configuration of the data acquisition equipments.
The type of rack should be set as either k41 if the combination of
model 7632A and 7631A is used, or k42 if the combination of model
7624 and 7623 is used. The type of recorder should be set as either
k41 if the DFC1100 is used, or k42 if the DFC2100 is used.
Next, data and control cables should be connected. The input
interface unit and the data recorder unit is connected with one
data cable (VCD cable: blue) and one control cable (RS-422 cable:
black). The data cable should be connected to the DATA OUT
connector of the input interface unit and to the DATA INPUT
connector of the data recorder unit. The control cable should be
connected to the TO DR connector of the input interface
unit and to the REMOTE 4 connector of the data recorder
unit. All the K-4 VLBI equipments are controlled via GP-IB data
communication bus from the FS9 host computer except for the data
recorder unit is actually controlled by the input interface unit
via RS-422 but all the communications from the FS9 host related
with the data recorder are done with the input interface unit.
Each unit has a switch to set the GP-IB address. After setting a
unique address to each unit, all the units should be connected to
the FS9 host computer by GP-IB cables. Total length of the GP-IB
cable should be kept as short as possible to prevent possible
communication troubles (GP-IB specification allows up to 20
meters in total). Then edit the /usr2/control/ibad.ctl
file and specify the configured GP-IB addresses. A sample file
is shown below.
In this example, the tape changer (tc) is set to the
address 2 and the input interface (d4) is set to the
address 4, etc. If the k41 rack is selected (i.e. model 7632A
local oscillator unit and model 7631A video converter unit),
'v4' and 'l4' are used to specify the GP-IB
addresses of the video converter and the local oscillator unit,
respectively. If the k42 rack is selected (i.e. model 7624
local oscillator unit and model 7623 video converter unit),
'va' and 'vb' are used to specify two GP-IB
addresses of the two video converter units, and, 'la'
and 'lb' are used to specify two GP-IB addresses of the
two local oscillator units.
Lastly, the file /usr2/control/dev.ctl should be edited
to reflect which GP-IB devices are used at the FS9 host
computer. Use 'board' for the GP-IB board device name
if a NI GP-IB communication board is used, and use
'/dev/ttyXX' if a GPIB-RS232C converter box is used where
XX depends on the actual configuration of the RS232C port
(S1 for com1 port for example).
4. Regular Operations
Once all the equipments are connected and
all the control
files are properly edited, run FS9 software and issue a
command rec=init from the FS9 console terminal.
If the configurations were correct, the time code on the
front panel of the input interface unit turns to all-zero
for about a second and then returns to the normal state.
This command initialize the unit and is often required
after the system configurations were modified. Then
execute tape command to check the data recorder unit,
vc and vclo commands to check the K41 type rack,
and va vb vcla vclb commands to check the K42 type
rack. If the configurations were correct, responses will be
shown in the log window.
If these commands did not work properly, be sure to update
the FS9 software to newer versions. The curreently available
official version does not support the K4 devices as of this
time, and the actual version which is required to use the
K4 VLBI system will be announced in the near future.
At the time of observations, a procedure file and a snap
command file have to be prepared by using DRUDG software
later than the version NRV980302.
The K-4 VLBI system and other VLBI systems can be connected
to the FS9 host computer simultaneously. Which system is
actually used can be switched by editing the equip.ctl
file. If one of the control files are modeified, fs
program must be restarted to make these changes effective.
5. Related Documents
Following is a list of related documentations. If you do not
have these documents, please request these documents to
koyama(AT)nict.go.jp
or to
weh(AT)vega.gsfc.nasa.gov.
Journal of the Communications Research Laboratory,
vol. 38 (1991), 'special issue on the results
of VLBI experiments at the Communications Research
Laboratory (1984-1990)'
IERS TDC News, issued biannually by
Communications Research Laboratory
Proceedings of the Technical Workshop for APT and
APSG, Kashima, December 1996
VLBI Software Documentation, Field System,
NASA/Goddard Space Flight Center, Space Geodesy
Program