[Difx-users] On delay modelling

Mugundhan vijayaraghavan v.vaishnav151190 at gmail.com
Mon Apr 24 00:41:55 EDT 2017


Dear Adam,

Thank you for your clarifications.

One more question:
The unit vector \hat(s) originates from the center of the earth, in this
case, the hour angles of the sources will have to be calculated as GMST-RA
? In this case, do we have to offset the obtained hour angles and the
declination by the lat and long of the observing stations ?

Thank you,

Mugundhan

On Mon, Apr 24, 2017 at 6:10 AM, Adam Deller <adeller at astro.swin.edu.au>
wrote:

> Hi Mugundhan,
>
> On 21 April 2017 at 15:30, Mugundhan vijayaraghavan <
> v.vaishnav151190 at gmail.com> wrote:
>
>> Dear All,
>>
>> I have a few queries about how delay modelling is carried out in VLBI for
>> compensating the same.
>>
>> 1.) The geometric delay is calculated as tg=*b.s*, where *b *is the
>> baseline vector and *s *is the source vector. Lets say I have two
>> antennas, both located about 100 kms apart. How do standard VLBI delay
>> modelling software calculate this delay ? Based on some preliminary reading
>> I understood that the baseline distance are first calculated referenced to
>> the earth center, if this is done, are delays estimated assuming the earth
>> center to be the phase reference ? How is this earth centered reference
>> then transformed to the celestial frame ? because both *b *and *s *must
>> be in the same coordinate system for carrying out a dot product operation,
>> right ?
>>
>
> VLBI delay modeling is very complicated, involving considerably more than
> just a *b.s* operation.  Other propagation effects are taken into account
> too, and the length of the baseline *b* is changing with time due to
> tidal forces and what-not, plus the whole system is wobbling around due to
> the changing earth orientation.
>
> But stripping it back to the minimum: yes, the Earth centre is usually
> used as the reference.  Look up the International Terrestrial Reference
> Frame (ITRF) to see the definition of the axes.  Then you obviously need to
> know the *time* (and the Earth orientation parameters) to figure out
> where the unit vector \hat(s) that points at the direction of the source is
> pointing in this reference frame.  For each telescope, we then compute the
> station-based delay from the telescope back to the geocentre at the desired
> instant of time, and each telescope's data stream is delayed by the
> computed amount (rather than shifting only one data stream by the
> difference between \tau_a and \tau_b).  That's what it means to use the
> geocentre as the reference.
>
>
>>
>> 2.) In some books/articles i find a reference to a RA and Dec of Baseline
>> ? What does this physically mean ? I'm not able to visualize this clearly.
>> any help will be greatly appreciated !
>>
>
> Like I said above, it makes more sense to figure out where the source unit
> vector is pointing relative to a telescope coordinate system.  You can
> equivalently rotate the telescope coordinates and keep the source unit
> vector fixed, but that is (I think) less intuitive.
>
>
>>
>> 3.) In the complete delay model, tm, which is the sum of geometric
>> delay+clock delay+ionospheric/atmospheric delay+fixed delays due to analog
>> component, the fastest varying component will be geometric delay only, once
>> this is compensated, if the other quantities are contributing to some
>> excess time varying delay, this will be seen as a residual fringe. Now, for
>> clock delay, is this estimated using the allan deviation of the clock being
>> used? Lets say my clock loses 10^-9 seconds in 30 minutes, and if I sample
>> my signal at 16 MHz which is ~ 62.5 ns, will I be able to integrate the
>> data without any degradation due to clock upto 30 minutes ?
>>
>>
> The sampling time is irrelevant.  It's the sky frequency that determines
> the visibility phase.  Your signal might only be 16 MHz wide, but if you
> were observing at 100 GHz then a change of 1 nanosecond translates to 100
> turns of phase.  So in that example you could only integrate for maximally
> a fraction of a second.  Normally VLBI clock drifts are monitored to a
> level of at worst a few ns/day or so. If they are unknown then a test
> correlation is performed to determine the clock offset and drift, and then
> the observation is recorrelated having applied the best available clock
> model.
>
>
>> 4.) There is also an associated baseline velocity component which will
>> lead to a time difference between the wavefronts received at both the
>> antennas. Is this baseline velocity the same as the orbital velocity of the
>> earth ? Or is this modelled differently ?
>>
>>
> By delay tracking to the geocentre, this problem is naturally taken into
> account. When you use the geocentre, you are automatically forced to
> account for the rotation of the reference frame between the time the signal
> is received at the antenna and the time that it would pass through the
> geocentre.  So you've corrected for the velocity of both of the stations,
> rather than their difference.  The process is known as retarded baseline
> correction.
>
> Unfortunately the documentation for VLBI delay packages is not extensive.
> You can look up CALC (https://lupus.gsfc.nasa.gov/software_calc_solve.htm)
> or VTD (http://astrogeo.org/vtd/) but neither have an excellent
> explanation of the theory.
>
> Cheers,
> Adam
>
>
>> I would greatly appreciate if the experts here clarify my doubts. Kindly
>> do point me to references that may lead to clarification of these doubts
>> too !
>>
>> Thanking you,
>> With best regards,
>>
>> Mugundhan V.
>>
>>
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>
>
> --
> !=============================================================!
> Dr. Adam Deller
> ARC Future Fellow, Senior Lecturer
> Centre for Astrophysics & Supercomputing
> Swinburne University of Technology
> John St, Hawthorn VIC 3122 Australia
> phone: +61 3 9214 5307 <+61%203%209214%205307>
> fax: +61 3 9214 8797 <+61%203%209214%208797>
>
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> !=============================================================!
>



-- 
the giver of moksha
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