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: http://www.iki.rssi.ru/interball/sts.html Дата изменения: Mon Mar 25 19:24:56 1996
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                 Onboard data collecting system (STS)

 Panska Ves Ionospheric and Telemetric Observatory
    In the INTERBALL project the ODCS version  was  chosen  as   the 
system of data collection (STS) since  this  version  together  with 
the STO  telemetry  on  the  main   satellite   provides   acceptably  
high resolution  in  real  time.  The  channel  of    digital    data  
transmission can operate with the  rate  up  to  40  Kbit/s  and  the 
channel of  analog information makes it possible to transmit the data 
with the band width up to 60 KHz.
 
    In this case it is especially important that the data received from both spacecraft would match in time with high accuracy, otherwise some approaches to interpreting  the  measurement  results 
would  be  impossible.  However,  for  long  distances   from   the  
Earth,the TM-rate (the band width) is rather limited.
 
    An  important  component  of  the  TM-system  is   the   digital  
onboard memory  device  with  the  capacity of 4  Mbyte  designed   for  
recording   the housekeeping  data  out  of  the  zone  of    the  
radio-visibility  from the ground-based stations and for  registering 
the scientific data  in several  operation  modes  depending  on  the 
measurement program. 
    The onboard data collecting unit, STS, is installed to   collect 
the analog and digital information from the  complex  of  scientific 
payload  and  from  the  subsatellite  service  systems.  This  unit 
performs also the formation of the digital TM frame structure. 
    STS unit has the following features: 
    1. STS can  operate  in  receiving/transmitting  modes   through  
14 digital and 15 analog channels (or  through  120  analog  channels  
with the use of multiplexer controlled by STS 3-bit parallel codes).
 
    2. STS includes the  onboard  computer  on  the  basis  of   the  
NSC-800 microprocessor. The onboard computer can   receive   digital  
data directly from scientific instrument and from  service  systems,  
and after the data processing sends the resulting digital data  both  
to the TM-frame (and, if needed, backward to the system) in the form 
of 8-bit words to control the  operation  modes  and   the   programs  
of operation of the instruments and systems.
 
    3. The rate of data  transmission  has  4  fixed  values:  1.23, 
5.12,20.48  and  40.96  kbit/s.   The   operative   rate   of   data  
transmission  is  valid  both  for  the  telemetry  and   for   data  
transmission  from  the onboard computer to instruments.
 
    4. The system has 8 prefixed  independent  TM-frame   structures 
and  gives  a  possibility  to  form   in  flight    an    arbitrary  
additional structure.  Each of  the  8  versions  of  the   TM-frame  
structures provide the optimum distribution of  the  TM  information  
in  a  block depending on particular conditions of  the   experiment  
and  on  the program of studies.
The largest information block in  the  STS  is  the  main  block 
(512bytes) consisting of 4 subframes of 128 bytes.
 
    The signal to transmitter from  the  STS  unit  output  has  the 
form of bi-phase modulation.
The following organizations took part in design of the data collecting system:
-Microvawe Department of the Budapest Technical University, Hungary;
-Geophysical Institute of the Czech Acad. Sci., Prague, Czech Republic;
-BL Electronics, Hungary;
-Institute of Atmospheric Physics of the Czech Acad. Sci., Prague, Czech Republic.
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