R3399 sbtx to molniya sat using gbt and vlba
oct19
preparing for the test
performing the experiment
rise,set times
tx power
Project r3399 is testing sband transmission to
satellites and then receiving at gbt and the vlba.
The dead russian satellites molniya were used for the targets.
transmission will occur on 27 and 28oct19.
Preparing for the test:
Creating the ephemeris
file
- I'm storing the info in /share/obs4/usr/radar/r3399/
- tle's were download from celestrak
- I've used the 19297.429 tle's
- tle.191027
- MOLNIYA 2-9
1 07276U 74026A 19297.42981504
.00000029 00000-0 67986-3 0 9992
2 07276 63.7779 20.5574 6843309
289.0551 12.3182 2.45095432225650
- tle.191028
- MOLNIYA 3-10
1 11057U 78095A 19297.80922998
.00001337 00000-0 18064-3 0 9994
2 11057 62.6564 50.5084 5979996
293.4621 16.1522 4.08988723344139
- The tle files should be named:
- tle.yymmdd (since mkephm.sc uses the
date to select the tle file).
- The routine mkephm.sc will generate an ao radar ephemeris from
the tle's
- edit mkephm.sc
- date=191027
- tmSt=1330
- tmEnd=1530
- date:yymmdd, tmSt=hhmm (start time), tmEnd=hhmm (end time)
- where dates and times are utc.. don't enter leading 0's in
the times
- ./mkephm.sc . this will
- send to tle file to horizons telnet interface
- download the ephemeris quantities: 2 (app
ra,dec) ,4(apparent az,el), 20(range and rangerate)
- run hortoao.pl to convert from horizons to ao short format
- run ephmaotordr to convert from ao short format to ao
radar
- The radar ephm will have the rx info equal to the tx info
- looking at the round trip time and the az,el change per
second this can introduce a pointing error of about 1"
- the doppler will be set to 0.
- Links to radar ephemeris files that
were used
- .297 used the 19297 tle files
- .299 used the 19299 tle files
Checking the az,za rates
Using the ephemeris file, i plotted up the
positions and rates of the satellites for each day
molniya position and rates for
27/28oct19 (.ps) (.pdf)
- Page 1-2 27oct19 molniya 2-9
- Page 3-4 28oct19 molniya 3-10
- FirstPage: az,za
- top: az,za track. rise is on the right
- This plots the feed azimuth (180 degrees from the source
azimuth)
- middle: az rate vs hour of day
- the dashed red lines are the slew rates in azimuth
- bottom: za velocity vs hour of day
- the dashed red lines are the slew rates
- 2nd page: ra,dec,rtt, sat velocity
- top is the apparent ra,dec track for the object.
- middle: round trip time (from, to AO) in millisecs
- bottom: satellite radial velocity (km/sec) with negative
approaching AO.
The
difference between the 297,299 tle files:
The tle files were downloaded from
celestrack.
- 27oct19 tracking:
- the tle file was dated 19297 (24oct19)
- It was downloaded friday 25oct19.
- a 19299 tle file was available on 26oct19 (but was not
used).
The plots show the position
differences for ephemerides made from the two tle files (.ps)
(.pdf)
- ephem299 - ephm297 is plotted
- Top: little circle az (black), za(red) differences vs
azimuth (source az)
- middle: great circle difference
- The max value is about 4 arc seconds.
- bottom :great circle difference vs hour (utc)
Summary:
- the positions only change be about 4 asecs between the
two dates
processing: x101/191027/chkephm.pro
Performing the experiment
We will probably start out with cw to make sure the other
stations see a signal
- rise/set times (utc)
- 27oct19 : 14:16:00 to 15:25:30
- 28oct19 : 15:34:00 to 16:08:00
Transmitted power
The plot shows the
transmitted power vs hour of day for 27,28oct19 (.ps) (.pdf)
processing: usr/radar/r3399/mkpehm.sc,
x101/191027/sbsat.pro,chkephm.pro,pwrlog.pro
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