On 6/16/17 10:55 PM, Lifespeed via time-nuts wrote:
Not too surprising to read locking two crystal oscillators together
without using a physical cable is difficult to impossible.
Essentially what I am looking for is the phase alignment accuracy
(and phase noise) one would get PLL’ing one oscillator to the other
using a cable, but over a longer distance. Some modest phase noise
degradation might be acceptable, but not an order of magnitude.
Clearly not a trivial problem. Yes, the jitter (phase noise)
typically accomplished from a PLL phase comparing at 100MHz is better
than what one could get “locking” to GPS. It was just a thought,
apparently not a realistic one. Thanks for disabusing me of that
notion.
Well, at JPL we regularly lock two crystal oscillators together that are
over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the
distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
So it is doable
The performance depends ultimately on the noise within your tracking
loop bandwidth.
Yes, one has to lock them at a high reference frequency so as to avoid multiplied-up phase noise. I can manage the tracking loop design. Some applications aren't line-of-sight, so the radio link doesn't solve every situation. Fiber optic backup plan, but everybody hates cords.
This is my application as well, phase measurement of the signals separated by some distance. Not a billion km, but even a few km requires similar considerations.
Lifespeed
-----Original Message-----
From: jimlux [mailto:jimlux@earthlink.net]
Well, at JPL we regularly lock two crystal oscillators together that are over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
So it is doable
The performance depends ultimately on the noise within your tracking loop bandwidth.
sorry about, but
who is 'lifespeed', a robot or a real person with a natural name?
many thanks,
73, Arnold, DK2WT
Am 17.06.2017 um 23:07 schrieb Lifespeed via time-nuts:
Yes, one has to lock them at a high reference frequency so as to avoid multiplied-up phase noise. I can manage the tracking loop design. Some applications aren't line-of-sight, so the radio link doesn't solve every situation. Fiber optic backup plan, but everybody hates cords.
This is my application as well, phase measurement of the signals separated by some distance. Not a billion km, but even a few km requires similar considerations.
Lifespeed
-----Original Message-----
From: jimlux [mailto:jimlux@earthlink.net]
Well, at JPL we regularly lock two crystal oscillators together that are over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
So it is doable
The performance depends ultimately on the noise within your tracking loop bandwidth.
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On Sat, 17 Jun 2017 06:29:02 -0700
jimlux jimlux@earthlink.net wrote:
Well, at JPL we regularly lock two crystal oscillators together that are
over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the
distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
This sounds interesing. What do I have to google for to learn more?
Attila Kinali
--
It is upon moral qualities that a society is ultimately founded. All
the prosperity and technological sophistication in the world is of no
use without that foundation.
-- Miss Matheson, The Diamond Age, Neil Stephenson
On 6/18/17 7:10 AM, Attila Kinali wrote:
On Sat, 17 Jun 2017 06:29:02 -0700
jimlux jimlux@earthlink.net wrote:
Well, at JPL we regularly lock two crystal oscillators together that are
over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the
distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
This sounds interesing. What do I have to google for to learn more?
It's just how we do radio science/ranging - you transmit a spectrally
pure signal from earth (typically oscillator locked to a maser), at the
spacecraft you have a very narrow band PLL (traditionally a VCXO) that
locks to the received signal, and you generate the downlink signal from
that same oscillator, transmit it back to earth, and compare.
The transmitted signal is precisely in a specified ratio with the
received signal (880/749 for X-band 7.15 GHz from earth, 8.4 GHz coming
back). For Ka-band, the earth signal goes up at 34 GHz, and comes back
at 32 GHz
A typical spec is that the transponder introduce no more than 4E-16 ADEV
at 1000 sec.
https://descanso.jpl.nasa.gov/ has links to a whole bunch of useful
references
https://descanso.jpl.nasa.gov/monograph/mono.html
specifically volume 1 by Thornton and Border talks all about radiometric
ranging.
The various design and performance series describe the specific
implementations.
Joe Yuen's "Deep Space Telecommunications Engineering"
https://descanso.jpl.nasa.gov/dstse/DSTSE.pdf
Chapter 3 covers receiver design
Chapter 4 covers radio tracking
--
Then you can look for papers on "deep space transponder" The classic
design papers are in the 90s. IEEE MTT, and the JPL IPN progress
reports.
The Cassini Deep Space Transponder is sort of a progenitor of them -
then there's the Small Deep Space Transponder (SDST) designed in the
90s, flying 2000 through now.
Somewhere around 2000, the design started moving away from trying to
lock the oscillator to doing the phase lock and phase/frequency
turnaround in a digital loop, with a fixed oscillator driving DDS or
NCO. At JPL, this would be the "Advanced Deep Space Transponder", but
Thales Alenia Space Italia (TASI) uses a similar approach for their deep
space transponders (look for Juno and BepiColombo)
Jim -
Your first thread in this post was fascinating to me - stuff I'd never been
exposed to. It seems like the 'tricks of the trade' for so much of how
things actually get done are so often only accessible to those who work
closely with them. I was about to shoot you an email to ask if there was
any reference (other than piles of journal articles) that cover some of
these topics, when I scrolled down and found this post with the Descanso
links and references. What a trove! There's more info in the links on
that page than I could ever hope to comprehend.
Many thanks for this post. It will remain marked and in the back of my
brain as "stuff that you should learn". If we only ever had enough time.
Why didn't anyone ever expose me to this stuff when I was young and just
starting in RF?
Brent
On Sun, Jun 18, 2017 at 1:36 PM, jimlux jimlux@earthlink.net wrote:
On 6/18/17 7:10 AM, Attila Kinali wrote:
On Sat, 17 Jun 2017 06:29:02 -0700
jimlux jimlux@earthlink.net wrote:
Well, at JPL we regularly lock two crystal oscillators together that are
over a billion km apart with added Allan deviation of less than 1E-15 at
1000 seconds with a radio link at 7.15 GHz. It's how we measure the
distance and velocity to spacecraft (a few cm in range and mm/s in
velocity) and from that figure out the gravitational fields (among other
things)
This sounds interesing. What do I have to google for to learn more?
It's just how we do radio science/ranging - you transmit a spectrally pure
signal from earth (typically oscillator locked to a maser), at the
spacecraft you have a very narrow band PLL (traditionally a VCXO) that
locks to the received signal, and you generate the downlink signal from
that same oscillator, transmit it back to earth, and compare.
The transmitted signal is precisely in a specified ratio with the received
signal (880/749 for X-band 7.15 GHz from earth, 8.4 GHz coming back). For
Ka-band, the earth signal goes up at 34 GHz, and comes back at 32 GHz
A typical spec is that the transponder introduce no more than 4E-16 ADEV
at 1000 sec.
https://descanso.jpl.nasa.gov/ has links to a whole bunch of useful
references
https://descanso.jpl.nasa.gov/monograph/mono.html
specifically volume 1 by Thornton and Border talks all about radiometric
ranging.
The various design and performance series describe the specific
implementations.
Joe Yuen's "Deep Space Telecommunications Engineering"
https://descanso.jpl.nasa.gov/dstse/DSTSE.pdf
Chapter 3 covers receiver design
Chapter 4 covers radio tracking
--
Then you can look for papers on "deep space transponder" The classic
design papers are in the 90s. IEEE MTT, and the JPL IPN progress reports.
The Cassini Deep Space Transponder is sort of a progenitor of them - then
there's the Small Deep Space Transponder (SDST) designed in the 90s, flying
2000 through now.
Somewhere around 2000, the design started moving away from trying to lock
the oscillator to doing the phase lock and phase/frequency turnaround in a
digital loop, with a fixed oscillator driving DDS or NCO. At JPL, this
would be the "Advanced Deep Space Transponder", but Thales Alenia Space
Italia (TASI) uses a similar approach for their deep space transponders
(look for Juno and BepiColombo)
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