Re: [time-nuts] GPS Usage

2011-03-09 Thread Poul-Henning Kamp
In message 55371.12.6.201.2.1299648580.squir...@popaccts.quikus.com, J. Fors
ter writes:

in reality more than 90 percent of the users of GPS worldwide use it
primarily for a timing reference.

That makes the LORAN shutdown look even more idiotiuc!

Well, how can you argue with closing a system that was aiding terrorists ?

The reason LORAN-C got killed was that DoD/DHS couldn't jam it if a
terrorist with a suitcase-nuke was trying to find his way to Congress.

Your government money at work...

-- 
Poul-Henning Kamp   | UNIX since Zilog Zeus 3.20
p...@freebsd.org | TCP/IP since RFC 956
FreeBSD committer   | BSD since 4.3-tahoe
Never attribute to malice what can adequately be explained by incompetence.

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Re: [time-nuts] GPS Usage

2011-03-09 Thread Hal Murray

p...@phk.freebsd.dk said:
 The reason LORAN-C got killed was that DoD/DHS couldn't jam it if a
 terrorist with a suitcase-nuke was trying to find his way to Congress. 

Why can't they jam it?

It's just a matter of signal strength.  If want to jam a small region, they 
can use a local transmitter.  If they want to disable a large region, they 
can turn off the transmitters or have them transmit garbage.


-- 
These are my opinions, not necessarily my employer's.  I hate spam.




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Re: [time-nuts] GPS Usage

2011-03-09 Thread Poul-Henning Kamp
In message 20110309082926.d5f9f800...@ip-64-139-1-69.sjc.megapath.net, Hal Mu
rray writes:

p...@phk.freebsd.dk said:
 The reason LORAN-C got killed was that DoD/DHS couldn't jam it if a
 terrorist with a suitcase-nuke was trying to find his way to Congress. 

Why can't they jam it?

They can, All the need is 3 truck mounted generators, a truck with
the electronics and then drape a superconducting loopantenna over
a couple of skyskrapers...

DHS was concerned this would not be immediately available in an
emergency, whereas pretty much any army or air-force base can deliver
GPS jamming on minuted notice.

-- 
Poul-Henning Kamp   | UNIX since Zilog Zeus 3.20
p...@freebsd.org | TCP/IP since RFC 956
FreeBSD committer   | BSD since 4.3-tahoe
Never attribute to malice what can adequately be explained by incompetence.

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Re: [time-nuts] GPS Usage

2011-03-09 Thread Javier Herrero

El 09/03/2011 06:29, J. Forster escribió:

This is a surprise:

in reality more than 90 percent of the users of GPS worldwide use it
primarily for a timing reference.


This is a phallacy, except if we are taking into account indirect GPS 
users, i.e. admitting that a credit card user is a GPS user because the 
timestamping of the translation relies on a GPS :) But I suspect that, 
except in our time-nuts laboratories, the percentage of GPS receivers 
dedicated to timing compared to those dedicated to positioning is really 
low. Also, sometimes GPS timing is used because it is unexpensive, but 
provides an accuracy orders of magnitude better than the real needs (a 
traffic control radar camera tags the pictures with a one second 
precision... but uses a GPS, could be tagged with microsecond precission 
;) ).


And anyway, in a no-GPS world with real mass high-precission timing 
needs, other methods could be used... that would suppose a higher demand 
of Cs clocks and H-masers (so we could buy a good user H-maser for 
USD100 at the place you all know? mmm... not so bad ;) )


--

Javier HerreroEMAIL: jherr...@hvsistemas.com
Chief Technology Officer
HV Sistemas S.L.  PHONE: +34 949 336 806
Los Charcones, 17 FAX:   +34 949 336 792
19170 El Casar - Guadalajara - Spain  WEB: http://www.hvsistemas.com


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Re: [time-nuts] GPS Usage

2011-03-09 Thread Poul-Henning Kamp
In message 4d7740b8.2040...@hvsistemas.es, Javier Herrero writes:
El 09/03/2011 06:29, J. Forster escribi=F3:
 This is a surprise:

 in reality more than 90 percent of the users of GPS worldwide use it
 primarily for a timing reference.


This is a phallacy, except if we are taking into account indirect GPS
users, 

By far the biggest one is cell-phone base stations, and since these
don't work without good timesync (See recent story about the Koreas)
I think it is fair to include the indirect users in the collateral
damage.

-- 
Poul-Henning Kamp   | UNIX since Zilog Zeus 3.20
p...@freebsd.org | TCP/IP since RFC 956
FreeBSD committer   | BSD since 4.3-tahoe
Never attribute to malice what can adequately be explained by incompetence.

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Re: [time-nuts] Low noise power supply

2011-03-09 Thread David C. Partridge
H I wasn't impressed.  The 'scope screen shot of noise levels on the 
outputs used 20mV/division, and the thickness of the regulated traces told us 
precisely nothing.  Now if the author had measured 20uV noise over a BW of 10Hz 
to 100kHz (about 63nV/rtHz), or 3uV over the same BW (about 10nV/rtHz), I'd 
have started to get interested.  

However as no claims were made, I took the title of Ultra-Low Noise with a 
large shovel of salt.   


Regards,
David Partridge


-Original Message-
From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On Behalf 
Of ewkeh...@aol.com
Sent: 08 March 2011 21:41
To: time-nuts@febo.com
Subject: [time-nuts] Low noise power supply

There is an interesting article in the March 2011 Electronic Products magazine 
design an ultra low noise supply for analog circuits. It is a combination of 
switcher and LDO's and written by P Hunter TI so it may also  be available on 
their site.
Bert Kehren
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Re: [time-nuts] Low noise power supply

2011-03-09 Thread ehydra
If one can say that the actual noise-floor signal is approx. white noise 
than the peak to average is a factor of 6 to 7 on a analog scope. I once 
read this somewhere and found it not a so bad decision.



- Henry

--
ehydra.dyndns.info



David C. Partridge schrieb:
H I wasn't impressed.  The 'scope screen shot of noise levels on the outputs used 20mV/division, and the thickness of the regulated traces told us precisely nothing.  Now if the author had measured 20uV noise over a BW of 10Hz to 100kHz (about 63nV/rtHz), or 3uV over the same BW (about 10nV/rtHz), I'd have started to get interested.  

However as no claims were made, I took the title of Ultra-Low Noise with a large shovel of salt.   



Regards,
David Partridge


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/8/11 9:57 AM, Kevin Watson wrote:

Hi Jim,

As part of my research into keeping time on rockets and spacecraft, I
joined
this list to see what I could learn from the masters. Of course I'm a
knuckle-head for not assuming that you'd be one of the resident masters
grin. Anyway, as my accuracy needs are modest (~10uS across many onboard
computers), have access to GPS most of the time and don't really need to
worry about relativistic effects (yet, anyway grin) or radiation effects
(due to redundancy), I thought I'd use a GPSDO that can handle a decent
amount of holdover and then use PTP to distribute time across the vehicle.
Do you, or anyone else, have a recomendation for the GPSDO? Jackson Labs'
(http://jackson-labs.com/) DROR seems like it might work, but I wonder if
there might be better alternatives.



I don't know that GPS is your big problem, more the holdover when you 
can't get a GPS signal because your antenna isn't pointed in the right 
direction or the high dynamics of the rocket cause it to loose lock.


So, you want sync to 10 microseconds over how long a time span?  1ppm 
would be 10 seconds, or are you looking at minutes or days?



And, do you need to sync to the outside world or just within your 
rocket/spacecraft?  That is, as long as local time stays synced, so 
that simultaneous events on different boxes are simultaneous, even if 
the local clock drifts, relative to UTC, that's ok.


I assume you're looking for small and relatively inexpensive, as opposed 
to just buying, say, a space qualified Rubidium reference from one of 
the various suppliers.


You also mentioned PTP... so you're interested in distributing time 
(or at least synchronization), and not adding extra wires for, e.g. IRIG 
timecode or a 1 pps.  PTP can certainly do the microsecond scale sync 
across Ethernet.  If you're using SpaceWire, the timecodes can get 
microsecond scale sync, as well.


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/8/11 11:41 AM, Chris Albertson wrote:

On Tue, Mar 8, 2011 at 9:57 AM, Kevin Watsontime-n...@enuuf.com  wrote:

Hi Jim,

As part of my research into keeping time on rockets and spacecraft, I joined
this list to see what I could learn from the masters. Of course I'm a
knuckle-head for not assuming that you'd be one of the resident masters
grin. Anyway, as my accuracy needs are modest (~10uS across many onboard
computers), have access to GPS most of the time and don't really need to
worry about relativistic effects (yet, anywaygrin) or radiation effects
(due to redundancy), I thought I'd use a GPSDO that can handle a decent
amount of holdover and then use PTP to distribute time across the vehicle.
Do you, or anyone else, have a recomendation for the GPSDO? Jackson Labs'
(http://jackson-labs.com/) DROR seems like it might work, but I wonder if
there might be better alternatives.


Off hand I'd worry a little about vibration.  How do crystals work
when being shaken with huge amount of mechanical and acoustic energy
during launch?


Oh, I'm sure that's just a matter of ordering the right oscillator, or 
packaging.  People launch optical payloads that can only tolerate a few 
Gs, so that's doable.  Unless you're doing something like mounting the 
oscillator on the engine grin...


The oscillator in your wristwatch or in a manpack radio probably sees a 
tougher environment, vibration wise, than most spacecraft gear.


There's already crystal controlled radios on rockets for things like 
range safety and telemetry, and I don't think they do anything 
particularly exotic.  On the other hand, they also probably don't try to 
do timing to nanoseconds, either.






Cooling.  Almost all commercial off the shelf gear depends on air and
has a maximum altitude at which it will operate.  Off gassing might be
a problem too if there is flux left on the PCB or even fingerprint oil
leftover from assembly.


yes and no.  Cooling of most leaded components is through the leads to 
the PC board. Cleaning takes care of outgassing, etc.   The Mars 
Pathfinder rovers used essentially off the shelf commercial radio modems 
that were cleaned by hand.






PTP is a new and not so mature technology so you will need to
characterize it on your own and likey port it so the specialized
processors you use your self


Well.. it's new compared to IRIG and NTP, but it has been around a 
while. However, given that the 1588 spec has had a couple significant 
revs, I suspect that interoperability might be dicey.


But the basic concept is pretty straightforward, and if you're 
implementing the ethernet PHY so you can get the hooks to the timing 
info, then you're in good shape.








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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/8/11 1:45 PM, Magnus Danielson wrote:

Kevin,

On 03/08/2011 06:57 PM, Kevin Watson wrote:

Hi Jim,

snip

Do you, or anyone else, have a recomendation for the GPSDO? Jackson Labs'
(http://jackson-labs.com/) DROR seems like it might work, but I wonder if
there might be better alternatives.


First thing to consider is that standard GPSes will not meet your needs,
since they have to obey the height and speed limits for export rules.



OTOH, if you're building a rocket that's big enough to need something 
like this, you can likely get the needed export licenses, or at least, 
comply with the export control laws.  But yes, the vanilla off the shelf 
GPS probably has the don't report over 60,000 ft or 1000 km/hr lockouts.







The side-effect is that doppler frequencies may be much higher and both
tracking and acquisition needs to include these more extremer doppler
frequencies.


That would be my concern with GPS... the so called high dynamic 
environment.  LEO orbit is 7km/sec, so you'd think the Doppler would be 
huge, but actually, that's not a big problem, since you already have to 
deal with an even higher Doppler from the GPS SVs already.   Whether 
your receivers nav solution can work with a fast moving platform is 
another story.  It may assume that nothing can go that fast, and so it 
doesn't track.


OTOH, if you're buying a GPS module from someone like Trimble or 
Motorola or whoever, you can probably ask them.






Use of PTP within a rocket or spacecraft may or may not be a good thing.
NMEA + PPS may suffice and be less power-hungry. IRIG may also be an
option.


I would agree.. unless you're trying to minimize wire count and you 
already have Ethernet.  Spacecraft designs are very mass and pin count 
sensitive (every pin in the connector needs to be tested, which costs 
money, etc.)


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Re: [time-nuts] GPS Usage

2011-03-09 Thread paul swed
OK really getting off topic
S without GPS timing Celphones would not work. How is this a bad thing?
That means the people talking and texting while driving, might actually stay
in their lanes.
Sounding pretty good to me.
We did not shut down Loran for some crazy plot. We did it to save the budget
and the world. That $36M was just killing the Obama administration.
With LORAN off we are greening the world, saving birds, improving the
economy and creating 1000s of new jobs. (I don't know about the last comment
but all of our politicians finish off every sentence with that comment).
Regard
Paul

On Wed, Mar 9, 2011 at 4:37 AM, Javier Herrero jherr...@hvsistemas.eswrote:



 By far the biggest one is cell-phone base stations, and since these
 don't work without good timesync (See recent story about the Koreas)
 I think it is fair to include the indirect users in the collateral
 damage.

  Yes... most collateral damages are ever inflinged to indirect users :)

 Regards,

 Javier


 --
 
 Javier HerreroEMAIL: jherr...@hvsistemas.com
 Chief Technology Officer
 HV Sistemas S.L.  PHONE: +34 949 336 806
 Los Charcones, 17 FAX:   +34 949 336 792
 19170 El Casar - Guadalajara - Spain  WEB: http://www.hvsistemas.com


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/8/11 11:05 PM, Magnus Danielson wrote:

On 03/09/2011 06:08 AM, Kevin Watson wrote:

Hi All. Thanks for responding. There are quite a few GPS receivers that
will work outside of the usual commercial-grade GPS limitations, but I'm
not too sure I need such a receiver. As my application is to just
accuratly time-tag messages for a data recorder, my thinking is to allow
a ruggedized GPSDO to stabilize on the pad before launch, and then just
before launch force the GPSDO into holdover mode and act as the PTP
grandmaster for the onboard computers until we reach orbit. Once on
orbit I have other means to synchronize the PTP grandmaster.


Why carry the dead weight of something unusable in orbit.

Drop the receiver and antenna out of the equation and just provide a
timing signal on launch pad...




I'm going to guess that you want a GPS receiver on orbit for other 
reasons (like to know where you are, if your IMU or star tracker dies)


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Re: [time-nuts] Low noise power supply

2011-03-09 Thread ehydra
For me, this looks like a advertisement campaign only. Not very 
sophisticated or ingenious. Read that you don't need LC-filters at the 
output because of the LDOs. *lol* If the designer ever heard of corner 
frequency??

And the ISL9000A is the same.


- Henry

--
ehydra.dyndns.info


David C. Partridge schrieb:
H I wasn't impressed.  The 'scope screen shot of noise levels on the outputs used 20mV/division, and the thickness of the regulated traces told us precisely nothing.  Now if the author had measured 20uV noise over a BW of 10Hz to 100kHz (about 63nV/rtHz), or 3uV over the same BW (about 10nV/rtHz), I'd have started to get interested.  

However as no claims were made, I took the title of Ultra-Low Noise with a large shovel of salt.   



Regards,
David Partridge


-Original Message-
From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On Behalf 
Of ewkeh...@aol.com
Sent: 08 March 2011 21:41
To: time-nuts@febo.com
Subject: [time-nuts] Low noise power supply

There is an interesting article in the March 2011 Electronic Products magazine 
design an ultra low noise supply for analog circuits. It is a combination of 
switcher and LDO's and written by P Hunter TI so it may also  be available on their 
site.
Bert Kehren
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Re: [time-nuts] Low noise power supply

2011-03-09 Thread J. Forster
Electronic Products is not a real engineering publication. It is a forum
purely for new product releases. Always has been.

Articles there are almost always written by applications engineers for the
product being touted.

I got it free for decades, and threw the magazine away at once, unread.

Why, you ask? Simple, the EEM...  Electronic Engineers' Master, the giant,
multi-volume industry directory with company names and phone numbers,
about the size of a cinder block... came free, with a subscription.

Best,

-John

=



 For me, this looks like a advertisement campaign only. Not very
 sophisticated or ingenious. Read that you don't need LC-filters at the
 output because of the LDOs. *lol* If the designer ever heard of corner
 frequency??
 And the ISL9000A is the same.


 - Henry

 --
 ehydra.dyndns.info


 David C. Partridge schrieb:
 H I wasn't impressed.  The 'scope screen shot of noise levels on the
 outputs used 20mV/division, and the thickness of the regulated traces
 told us precisely nothing.  Now if the author had measured 20uV noise
 over a BW of 10Hz to 100kHz (about 63nV/rtHz), or 3uV over the same BW
 (about 10nV/rtHz), I'd have started to get interested.

 However as no claims were made, I took the title of Ultra-Low Noise
 with a large shovel of salt.


 Regards,
 David Partridge


 -Original Message-
 From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On
 Behalf Of ewkeh...@aol.com
 Sent: 08 March 2011 21:41
 To: time-nuts@febo.com
 Subject: [time-nuts] Low noise power supply

 There is an interesting article in the March 2011 Electronic Products
 magazine design an ultra low noise supply for analog circuits. It is a
 combination of switcher and LDO's and written by P Hunter TI so it may
 also  be available on their site.
 Bert Kehren
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Re: [time-nuts] Low noise power supply

2011-03-09 Thread ehydra

Hi John and group -

For us germans, american magazines always look overloaded with 
advertisments. The marketenders don't like to hear that the generations 
under 40-50 are mostly advertisment blind just by natural adaption.
The times where I read paper electronics are long gone. The Internet 
completely took over. Sometimes I go for wooden pdfs in the local 
university library.


But back to the interesting subject - that I personally not fully 
resolved so there is a need of discussion!

Here is a first insight:
http://waltjung.org/PDFs/Sources_101_P2.pdf

In general: LDO is bad. low Iq is bad too.

cheers -
Henry


--
ehydra.dyndns.info


J. Forster schrieb:

Electronic Products is not a real engineering publication. It is a forum
purely for new product releases. Always has been.

Articles there are almost always written by applications engineers for the
product being touted.

I got it free for decades, and threw the magazine away at once, unread.

Why, you ask? Simple, the EEM...  Electronic Engineers' Master, the giant,
multi-volume industry directory with company names and phone numbers,
about the size of a cinder block... came free, with a subscription.

Best,

-John



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Re: [time-nuts] GPS Usage

2011-03-09 Thread jimlux


Lots of people use GPS for timing because it's cheaper or more 
convenient in a budgetary sens than alternate approaches.  Here at JPL, 
it's easier, in general, for me to put a GPS timing receiver and GPSDO 
in a lab than it is to try and run cables from the house sources.


The latter requires involvement of more facilities folks and touching 
more organizations (e.g. the people who send the signal, the people 
who maintain the wires or fiber, etc.), many of whom will have some 
sort of continuing charge (which is reasonable.. they ARE providing a 
service), for which you need a valid charge number.


Putting a GPSDO in a lab requires a one-time purchase and a one time 
facility request to put the antenna in.


We did a bit of an informal trade a few years back to look at 4 
alternatives for a half dozen labs in our building.


1) Distribute frequency standard and derived time code from JPL 
Frequency/Timing Lab (the maser)
2) Install a single GPSDO, and distribute the frequency reference and 
timecode
3) Install a single antenna, splitter, and install a separate GPSDO in 
each lab

4) Install multiple antennas and GPSDOs, one set for each lab.


the latter is the most flexible, and has the smallest individual 
increment cost (i.e. there's no capital improvement going on)


Given the plethora of GPS antennas sprouting from the tops of buildings 
around here, I suspect others have made similar analyses.


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Kevin Watson

Magnus,


Drop the receiver and antenna out of the equation and
just provide a timing signal on launch pad...


I need to keep computers time synchronized from launch through at least 
arrival on orbit so that time-tagged network messages can be played back 
with some degree of fidelity. For this, I need the time source on the 
rocket. Using a GPSDO in holdover mode seems like a good solution.


-Kevin


- Original Message - 
From: Magnus Danielson mag...@rubidium.dyndns.org

To: time-nuts@febo.com
Sent: Tuesday, March 08, 2011 11:05 PM
Subject: Re: [time-nuts] Spacecraft Timekeeping



On 03/09/2011 06:08 AM, Kevin Watson wrote:

Hi All. Thanks for responding. There are quite a few GPS receivers that
will work outside of the usual commercial-grade GPS limitations, but I'm
not too sure I need such a receiver. As my application is to just
accuratly time-tag messages for a data recorder, my thinking is to allow
a ruggedized GPSDO to stabilize on the pad before launch, and then just
before launch force the GPSDO into holdover mode and act as the PTP
grandmaster for the onboard computers until we reach orbit. Once on
orbit I have other means to synchronize the PTP grandmaster.


Why carry the dead weight of something unusable in orbit.

Drop the receiver and antenna out of the equation and just provide a 
timing signal on launch pad...


Cheers,
Magnus

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Kevin Watson

Jim,

I guess I should also have mentioned that I want to synchronize events 
across the rockets with those happening in our mission operations, and thus 
need a common time source. Furthermore, this is currently just an 
experiment, and is not safety or mission critical. We have other GPS units 
on board that can track all the way to orbit, but they're used for 
navigation, not time keeping. BTW, you can get oscillators that can 
withstand 30, 000 gs of shock. The Q-Tech QT88 is one example.


-Kevin

- Original Message - 
From: jimlux jim...@earthlink.net

To: time-nuts@febo.com
Sent: Wednesday, March 09, 2011 6:15 AM
Subject: Re: [time-nuts] Spacecraft Timekeeping



On 3/8/11 11:05 PM, Magnus Danielson wrote:

On 03/09/2011 06:08 AM, Kevin Watson wrote:

Hi All. Thanks for responding. There are quite a few GPS receivers that
will work outside of the usual commercial-grade GPS limitations, but I'm
not too sure I need such a receiver. As my application is to just
accuratly time-tag messages for a data recorder, my thinking is to allow
a ruggedized GPSDO to stabilize on the pad before launch, and then just
before launch force the GPSDO into holdover mode and act as the PTP
grandmaster for the onboard computers until we reach orbit. Once on
orbit I have other means to synchronize the PTP grandmaster.


Why carry the dead weight of something unusable in orbit.

Drop the receiver and antenna out of the equation and just provide a
timing signal on launch pad...




I'm going to guess that you want a GPS receiver on orbit for other reasons 
(like to know where you are, if your IMU or star tracker dies)


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Magnus Danielson

On 03/09/2011 03:09 PM, jimlux wrote:

On 3/8/11 1:45 PM, Magnus Danielson wrote:

Kevin,

On 03/08/2011 06:57 PM, Kevin Watson wrote:

Hi Jim,

snip

Do you, or anyone else, have a recomendation for the GPSDO? Jackson
Labs'
(http://jackson-labs.com/) DROR seems like it might work, but I
wonder if
there might be better alternatives.


First thing to consider is that standard GPSes will not meet your needs,
since they have to obey the height and speed limits for export rules.



OTOH, if you're building a rocket that's big enough to need something
like this, you can likely get the needed export licenses, or at least,
comply with the export control laws. But yes, the vanilla off the shelf
GPS probably has the don't report over 60,000 ft or 1000 km/hr lockouts.


Considering the linked GPS, I just wanted to make the point that a 
standard off the shelf civilian GPS won't cut it, unless it's for launch 
pad use only.



The side-effect is that doppler frequencies may be much higher and both
tracking and acquisition needs to include these more extremer doppler
frequencies.


That would be my concern with GPS... the so called high dynamic
environment. LEO orbit is 7km/sec, so you'd think the Doppler would be
huge, but actually, that's not a big problem, since you already have to
deal with an even higher Doppler from the GPS SVs already. Whether your
receivers nav solution can work with a fast moving platform is another
story. It may assume that nothing can go that fast, and so it doesn't
track.

OTOH, if you're buying a GPS module from someone like Trimble or
Motorola or whoever, you can probably ask them.


I was trying to point out issues beyond that of export limitations where 
a normal civilian GPS would not quite cut it. There is many such issues.



Use of PTP within a rocket or spacecraft may or may not be a good thing.
NMEA + PPS may suffice and be less power-hungry. IRIG may also be an
option.


I would agree.. unless you're trying to minimize wire count and you
already have Ethernet. Spacecraft designs are very mass and pin count
sensitive (every pin in the connector needs to be tested, which costs
money, etc.)


If you only run fast ethernet, you can use spare pins for whatever 
signal you like.


Cheers,
Magnus

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Magnus Danielson

On 03/09/2011 03:15 PM, jimlux wrote:

On 3/8/11 11:05 PM, Magnus Danielson wrote:

On 03/09/2011 06:08 AM, Kevin Watson wrote:

Hi All. Thanks for responding. There are quite a few GPS receivers that
will work outside of the usual commercial-grade GPS limitations, but I'm
not too sure I need such a receiver. As my application is to just
accuratly time-tag messages for a data recorder, my thinking is to allow
a ruggedized GPSDO to stabilize on the pad before launch, and then just
before launch force the GPSDO into holdover mode and act as the PTP
grandmaster for the onboard computers until we reach orbit. Once on
orbit I have other means to synchronize the PTP grandmaster.


Why carry the dead weight of something unusable in orbit.

Drop the receiver and antenna out of the equation and just provide a
timing signal on launch pad...




I'm going to guess that you want a GPS receiver on orbit for other
reasons (like to know where you are, if your IMU or star tracker dies)


Notice his last sentence...

I agree that there are many uses for a GPS onboard a sat... and if one 
wants one it needs to handle the altitude, speed, different amount of 
atmospheric shift, etc. etc. etc.


But if he only wants a GPS for launch pad synchronisation and then 
reverts to other methods, it seems like dead weight to bring it all the 
way up.


Cheers,
Magnus

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Magnus Danielson

Kevin,

On 03/09/2011 06:39 PM, Kevin Watson wrote:

Magnus,


Drop the receiver and antenna out of the equation and
just provide a timing signal on launch pad...


I need to keep computers time synchronized from launch through at least
arrival on orbit so that time-tagged network messages can be played back
with some degree of fidelity. For this, I need the time source on the
rocket. Using a GPSDO in holdover mode seems like a good solution.


If you only need to synchronise on launch pad, then you can separate off 
the OCXO and training logic (TIC, CPU and DAC) from the GPS receiver and 
antenna. Then you run in hold-over mode using the pieces you need. You 
then use the same core for whatever other method you use.


If you use a space-capable GPS receiver, then just hook in.

Cheers,
Magnus

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Kevin Watson

Hi Magnus,

As I said in an earlier message, this is an experiment that I want to run 
and would rather not touch mission and safety-critical GNC components, like 
our navigation GPS receivers. Mass is not an issue.


-Kevin

- Original Message - 
From: Magnus Danielson mag...@rubidium.dyndns.org

To: time-nuts@febo.com
Sent: Wednesday, March 09, 2011 10:25 AM
Subject: Re: [time-nuts] Spacecraft Timekeeping



Kevin,

On 03/09/2011 06:39 PM, Kevin Watson wrote:

Magnus,


Drop the receiver and antenna out of the equation and
just provide a timing signal on launch pad...


I need to keep computers time synchronized from launch through at least
arrival on orbit so that time-tagged network messages can be played back
with some degree of fidelity. For this, I need the time source on the
rocket. Using a GPSDO in holdover mode seems like a good solution.


If you only need to synchronise on launch pad, then you can separate off 
the OCXO and training logic (TIC, CPU and DAC) from the GPS receiver and 
antenna. Then you run in hold-over mode using the pieces you need. You 
then use the same core for whatever other method you use.


If you use a space-capable GPS receiver, then just hook in.

Cheers,
Magnus

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[time-nuts] difference between Oncore M12 and M12+T (useful when buying online)

2011-03-09 Thread Rick Hambly (W2GPS)

Every now and then I see e-mails like these. I would like to remind everyone 
that Synergy Systems, the USA distributor for the M12 series receivers, offers 
Ham Radio and Educational (time nuts) users a new M12M with the precision time 
firmware and an on board battery for only $59.18 with the 10% Ham/Edu discount 
(sown from $65.75). This unit also includes both Motorola binary and NMEA 
message formats. 

Synergy can be found at www.synergy-gps.com or at (858) 566-0666. They have 
been very good to the Ham and educational communities for many years.

Rick
W2GPS

-Original Message-
From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On
Behalf Of paul swed
Sent: Saturday, March 05, 2011 3:06 PM
To: Discussion of precise time and frequency measurement
Subject: Re: [time-nuts] difference between Oncore M12 and M12+T (useful
when buying online)

Indeed its not easy to tell whats, what either until you paid for it.
I purchased from Fluke.I and my modules is a M12 +. But who knows maybe
I was just lucky.
Regards
Paul
WB8TSL

On Sat, Mar 5, 2011 at 5:15 PM, John Beale be...@bealecorner.com
wrote:

 In case anyone else is shopping online for a used Motorola Oncore 
 M12+T timing GPS, it's probably useful to know what I just learned:

 Some online sellers offering M12+T 100 pps GPS may instead send you 
 a M12 Navigation (non-timing) GPS. The differences:

 Motorola Oncore M12 Navigation GPS:
 ---
 * Supports Motorola Binary and NMEA output
 * does not have 100 Hz output
 * does not have TRAIM (Timing Receiver Autonomous Integrity Monitor)
 * does not have sawtooth correction output
 * 1 PPS 500 ns timing

 crystal nearest MMCX antenna connector is two-lead can style with bent

 leads for surface mounting
 example p/n label: P183T12N12   (final N = Navigation?)

 photos:
 http://www.wa5rrn.com/GPS%20Other/Motorola%20M12/m12.pdf
 https://picasaweb.google.com/bealevideo/GPS#5580118907079326290

 Motorola Oncore M12+T Timing GPS:
 ---
 * Supports Motorola Binary output only
 * 1 Hz or 100 Hz output selectable
 * TRAIM (Timing Receiver Autonomous Integrity Monitor)
 * sawtooth correction (clock granularity) message available
 * 1 pps 2nS 1 Sigma, 6nS 6 Sigma (using sawtooth correction message)
 * 1 pps 10nS 1 Sigma, 20nS 6 Sigma (without correction)

 smaller leadless surface-mount crystals
 example p/n label: P283T12T17(final T = Timing?)

 photos:
 http://www.wa5rrn.com/GPS%20Other/Motorola%20M12/m12plusbrochure.pdf
 http://cgi.ebay.co.uk/ws/eBayISAPI.dll?VISuperSizeitem=290308535362

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Magnus Danielson

On 03/09/2011 07:58 PM, Kevin Watson wrote:

Hi Magnus,

As I said in an earlier message, this is an experiment that I want to
run and would rather not touch mission and safety-critical GNC
components, like our navigation GPS receivers. Mass is not an issue.


In that case, take a Thunderbolt, replace the OCXO with a more vibration 
tolerant variant, slap an antenna on the top, force it to hold-over mode 
just before launch and you are all done.


For best performance you want to tune up the Thunderbolt parameters to 
the new OCXO, which is a nice static exercise.


For a test it would suffice.

Cheers,
Magnus

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/9/11 10:58 AM, Kevin Watson wrote:

Hi Magnus,

As I said in an earlier message, this is an experiment that I want to
run and would rather not touch mission and safety-critical GNC
components, like our navigation GPS receivers. Mass is not an issue.

-Kevin


So this makes it pretty simple..

You have a GPS receiver that operates on the pad to get initial sync 
(and perhaps to calibrate your onboard oscillator... you don't actually 
need to discipline it, just have knowledge)


Then, you launch, and do your timestamping with the oscillator...

When you get on orbit, and your GPS reacquires, you can recalibrate or 
resync.


For that matter, what you could do is very simple.. run your oscillator 
and run a counter.  Snapshot the value of the counter every time you get 
a 1pps tick from the GPS.  Log the time/position/status messages from 
the GPS as well.


You can then fairly easily post process to back-out the variations in 
your oscillator (which will be small) and recalibrate your timestamps to 
UTC.


Now.. if you need to have different *spacecraft* be synchronized, the 
post processing scheme won't work.



A separate issue is the onboard distribution of time to 10 
microseconds.  PTP over Ethernet, SpaceWire Timecodes, or IRIG on a wire 
would meet that easily.



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Re: [time-nuts] difference between Oncore M12 and M12+T (useful when buying online)

2011-03-09 Thread ehydra

This is an alternative:
http://shop-emea.u-blox.com/abashop?s=274p=productdetailsku=553

Nice, as you can program it for PPS at 10KHz or some other frequency.

- Henry

--
ehydra.dyndns.info


Rick Hambly (W2GPS) schrieb:
Every now and then I see e-mails like these. I would like to remind everyone that Synergy Systems, the USA distributor for the M12 series receivers, offers Ham Radio and Educational (time nuts) users a new M12M with the precision time firmware and an on board battery for only $59.18 with the 10% Ham/Edu discount (sown from $65.75). This unit also includes both Motorola binary and NMEA message formats. 


Synergy can be found at www.synergy-gps.com or at (858) 566-0666. They have 
been very good to the Ham and educational communities for many years.

Rick
W2GPS



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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread Jim Kusznir
It has Demodulated IRIG as its main IRIG output, but it does have
one Modulated IRIG.  Others have told me I want the Modulated IRIG; I
honestly don't know what the differences are, and I haven't gotten out
a scope to see.

--Jim

On Tue, Mar 8, 2011 at 4:25 AM, Rob Kimberley r...@timing-consultants.com 
wrote:
 I looked at the data sheet of the sel-2407 and interestingly it states
 demodulated IRIG-B, which seems a bit odd. Either it's a modulated code
 i.e. a sinusoidal wave with amplitude modulation (usually about 3:1), or
 it's what we call a DC code i.e pulse width data stream not superimposed on
 the 1 KHz carrier.

 Rob Kimberley





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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Javier Herrero

Hello,

El 09/03/2011 19:58, Kevin Watson escribió:


As I said in an earlier message, this is an experiment that I want to 
run and would rather not touch mission and safety-critical GNC 
components, like our navigation GPS receivers. Mass is not an issue.


So I understand that timing is not distributed (or at least not 
available to you) in the spacecraft, that's a pity... I've seen in some 
spacecrafts that time is distributed using a PPS signal and a 
broadcasted message through MIL-1553 bus - would be a lot easier if you 
could hang to it (in the cases I know, it was a MIL bus only for the 
science payload TCs  HKs - independent from the GNC MIL bus). At least 
you're lucky since mass is not an issue (I've met people that would have 
killed for and aditional kg)


Regards,

Javier

--

Javier HerreroEMAIL: jherr...@hvsistemas.com
Chief Technology Officer
HV Sistemas S.L.  PHONE: +34 949 336 806
Los Charcones, 17 FAX:   +34 949 336 792
19170 El Casar - Guadalajara - Spain  WEB: http://www.hvsistemas.com


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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread Jim Kusznir
Thanks for the info!

I was adjusting the levels with alsamixer, which I suspect is a
digital mixer.  I hadn't thought of the potential issues there.

I was using the onboard sound, but I also have a higher quality
Soundblaster sound card.  Do some of these vary in quality so much as
to be unable to decode IRIG at all?

I think I will deploy PPS; I'd also like to deploy something to set my
time myself (IRIG sounds good), but I realize its not required.  I
haven't taken time to find all the connector-pieces to make the
required custom cable yet to do PPS; I had the parts on my shelf to
dump IRIG into my Line In on the sound card.

A related question:  for my IRIG out, should I directly dump that into
the sound card, use one BNC-T with a terminator, or two BNC-T's with
terminators, and pull the connection there?  Does it matter?

Thanks!
--Jim

On Mon, Mar 7, 2011 at 11:36 AM, Chris Albertson
albertson.ch...@gmail.com wrote:
 There is an NTP email list.   questi...@lists.ntp.org

 But really, all you need is the 1PPS output and some pool servers.
 If you have PPS working then all you need is a way to number the
 seconds and anything can do that.  Yes the PPS driver works with
 other non-NMEA ref clocks

 It would be good to get IRIG working.  One thing you don't say is how
 you are adjusting the levels.   Is it a digital control or an analog?
 In general you want to keep any digital control at maximum.  Reducing
 it even a little causes loss of dymanic range and reduces the
 effective with (number of bits) of the sample.  In the extream case
 your nice 24 bit WAV file is turned into 4-bit wide samples.   Such is
 the nature of integer math.

 Also if you are using the bui8lt-in sound on some PC, quality varies a
 lot. I'd start with a quality external audio interface.  But eiother
 way.  I think the first step is to look at the audio.  capture some to
 a file then look at the waveform using an audio editor.  Check for a
 reasonable amplitude with no clipping.  You will need to adjust the
 analog gain to get a good signa


 --
 =
 Chris Albertson
 Redondo Beach, California

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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread Jim Kusznir
My clock generates a couple variants of IRIG-B.  I wasn't able to find
docs on what variant of IRIG-B that NTP expects.  I know one variant
(which I tested, but am not using, nor do I expect to work) is high
precision, and is supposed to include the same accuracy as standard
IRIG-B + 1kPPS.

--Jim

On Mon, Mar 7, 2011 at 12:42 PM, Russell Rezaian rreza...@motorola.com wrote:
 This may sound a bit basic, so apologies if you have already passed this
 particular hurdle, but there are several different types of IRIG time code.
  A number of the clocks I have which generate IRIG can generate different
 versions of IRIG (e.g. IRIG B, IRIG H)

 If memory serves, the NTP code expects IRIG B.

 Have you confirmed that's what your clock is currently configured to
 generate?
 --
 Russell

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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread Russell Rezaian
IRIG is sometimes provided as a digital code at something useful for 
directly driving logic (I've seen this intended to drive TTL), and as 
the same digital code amplitude modulating an audio frequency carrier.


The modulated audio is the kind of IRIG that is usually decoded by 
the sound card input decoders.


It's also pretty easy to put on a track on mag tape, which was a very 
common use in days gone past when you could still get mag tape and 
people still used it for instrument data recording.


The demodulated IRIG sounds like the simple digital signal, and I'd 
guess you clock generates something that might be intended to drive 
some sort of digital logic, probably TTL.


I strongly suspect you'll get better results with the modulated 
IRIG using the NTP code and a sound card decoder.

--
Russell

At 11:35 AM -0800 2011/03/09, Jim Kusznir wrote:

It has Demodulated IRIG as its main IRIG output, but it does have
one Modulated IRIG.  Others have told me I want the Modulated IRIG; I
honestly don't know what the differences are, and I haven't gotten out
a scope to see.

--Jim

On Tue, Mar 8, 2011 at 4:25 AM, Rob Kimberley 
r...@timing-consultants.com wrote:

 I looked at the data sheet of the sel-2407 and interestingly it states
 demodulated IRIG-B, which seems a bit odd. Either it's a modulated code
 i.e. a sinusoidal wave with amplitude modulation (usually about 3:1), or
 it's what we call a DC code i.e pulse width data stream not superimposed on
 the 1 KHz carrier.

 Rob Kimberley





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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread Russell Rezaian

Hi Jim,


From what you've described, I think you need to use the modulated IRIG output.


I sent a previous email to that effect.

The audio card IRIG drivers expect IRIG B data 
used to modulate an audio carrier (AM).

--
Russell

At 11:42 AM -0800 2011/03/09, Jim Kusznir wrote:

My clock generates a couple variants of IRIG-B.  I wasn't able to find
docs on what variant of IRIG-B that NTP expects.  I know one variant
(which I tested, but am not using, nor do I expect to work) is high
precision, and is supposed to include the same accuracy as standard
IRIG-B + 1kPPS.

--Jim

On Mon, Mar 7, 2011 at 12:42 PM, Russell Rezaian 
rreza...@motorola.com wrote:

 This may sound a bit basic, so apologies if you have already passed this
 particular hurdle, but there are several different types of IRIG time code.
  A number of the clocks I have which generate IRIG can generate different
 versions of IRIG (e.g. IRIG B, IRIG H)

 If memory serves, the NTP code expects IRIG B.

 Have you confirmed that's what your clock is currently configured to
 generate?
 --
 Russell

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread John Nordlie

If there are already other GPS units onboard,
also be careful of interference.  On some of our
balloon work we have had COTS GPS receivers that
would jam each other if placed to closely together.

It'd be a shame if your $50 cheapie jammed the
space-rated unit and sank the whole mission.

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Re: [time-nuts] NTP IRIG config help

2011-03-09 Thread jimlux

On 3/9/11 11:40 AM, Jim Kusznir wrote:

Thanks for the info!

I was adjusting the levels with alsamixer, which I suspect is a
digital mixer.  I hadn't thought of the potential issues there.

I was using the onboard sound, but I also have a higher quality
Soundblaster sound card.  Do some of these vary in quality so much as
to be unable to decode IRIG at all?



I doubt sound card quality makes any difference for IRIG.. it's a low 
bandwidth low dynamic range signal that doesn't require extreme fidelity.




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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Tom Van Baak

Magnus,


Drop the receiver and antenna out of the equation and
just provide a timing signal on launch pad...


I need to keep computers time synchronized from launch through at least 
arrival on orbit so that time-tagged network messages can be played back 
with some degree of fidelity. For this, I need the time source on the 
rocket. Using a GPSDO in holdover mode seems like a good solution.


-Kevin


Some GPSDO learn their hold-over parameters over time,
sometime days, in which case you may be in for a surprise.

Is there any way you can simulate the temperature, vibration,
and g-force (or lack of) trauma that the GPSDO is going to
experience during this hour of launch-to-orbit?

If not,  I suggest a simple test: just throw your GPSDO and
battery in a backpack and go jogging. Twirl the backpack in
the air every now and then. After an hour I'd be very curious
by how many microseconds it's off.

/tvb


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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread SAIDJACK
Hi Tom, Kevin,
 
the JLT DROR GPSDO mentioned by Kevin in the original  email may be 
overkill for this application, as it is designed to provide  very low phase 
noise 
under extreme vibration conditions, and it  is state-of-the-art technology 
and priced accordingly. It is designed to  interface directly with a vehicle 
power supply, so that may help in simplifying  the installation.
 
Phase Noise doesn't seem to be a requirement here, and we do have a  
standard version that does not have the phase-noise-under-vibration cleanup  
loop installed to save substantial cost. It should work quite well in the  
application, as it has various extremely low-g-sensitivity oscillators on board 
 
that will keep drift to very small values even under very large 
acceleration and  vibration, and temperature changes. It was designed to be 
essentially 
 indestructible.
 
If cost is an issue, we have ultra-low-g versions of our FireFly-IIA  
products available (our g-force product line) that are designed and tested to  
provide a guaranteed holdover under the conditions that Tom mentions below. 
They  are designed to guarantee drift in backpack type applications without 
GPS, but  with lot's of thermal changes and a very wide temp range, loads of 
acceleration  (shock, vibration, and tilt), and fast warmup. To give an 
example, we can  achieve better than 0.1ppb per g per axis acceleration 
sensitivity on the  worst-case axis on our g-force products.
 
So for example the FireFly-IIA g-force would have the following drift in a  
hypothetical high-g application:
 
  g-force on average over entire trip - 3g (this extreme acceleration  
would never happen in reality of course)
  average thermal change - 40 Degrees C
  allowed warmup time with GPS - 1 hour
 
Drift over 5 hour mission:
 
   3g x 0.1ppb/g + 40C * 0.005ppb/C + 0.1ppb initial error =  0.6ppb 
overall average error over 5 hours
 
So in this extreme scenario we have 0.6ppb * 5 * 3600 = 10.8 microsecond  
drift over 5 hours.
 
Aging and retrace is not taken into consideration here, but that should be  
more than compensated by the unrealistic constant 3g acceleration error we 
added  to the calculation.
 
The cost of our g-force products is only about 2x to 2.5x the price  of our 
standard DOCXO products.
 
bye,
Said
 
 
 
 
In a message dated 3/9/2011 12:11:49 Pacific Standard Time,  
t...@leapsecond.com writes:

Some  GPSDO learn their hold-over parameters over time,
sometime days, in which  case you may be in for a surprise.

Is there any way you can simulate  the temperature, vibration,
and g-force (or lack of) trauma that the GPSDO  is going to
experience during this hour of launch-to-orbit?

If  not,  I suggest a simple test: just throw your GPSDO and
battery in a  backpack and go jogging. Twirl the backpack in
the air every now and then.  After an hour I'd be very curious
by how many microseconds it's  off.

/tvb


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Re: [time-nuts] difference between Oncore M12 and M12+T (useful when buying online)

2011-03-09 Thread paul swed
Thanks Rick had no idea

On Wed, Mar 9, 2011 at 2:04 PM, Rick Hambly (W2GPS) w2...@cnssys.comwrote:


 Every now and then I see e-mails like these. I would like to remind
 everyone that Synergy Systems, the USA distributor for the M12 series
 receivers, offers Ham Radio and Educational (time nuts) users a new M12M
 with the precision time firmware and an on board battery for only $59.18
 with the 10% Ham/Edu discount (sown from $65.75). This unit also includes
 both Motorola binary and NMEA message formats.

 Synergy can be found at www.synergy-gps.com or at (858) 566-0666. They
 have been very good to the Ham and educational communities for many years.

 Rick
 W2GPS

 -Original Message-
 From: time-nuts-boun...@febo.com [mailto:time-nuts-boun...@febo.com] On
 Behalf Of paul swed
 Sent: Saturday, March 05, 2011 3:06 PM
 To: Discussion of precise time and frequency measurement
 Subject: Re: [time-nuts] difference between Oncore M12 and M12+T (useful
 when buying online)

 Indeed its not easy to tell whats, what either until you paid for it.
 I purchased from Fluke.I and my modules is a M12 +. But who knows maybe
 I was just lucky.
 Regards
 Paul
 WB8TSL

 On Sat, Mar 5, 2011 at 5:15 PM, John Beale be...@bealecorner.com
 wrote:

  In case anyone else is shopping online for a used Motorola Oncore
  M12+T timing GPS, it's probably useful to know what I just learned:
 
  Some online sellers offering M12+T 100 pps GPS may instead send you
  a M12 Navigation (non-timing) GPS. The differences:
 
  Motorola Oncore M12 Navigation GPS:
  ---
  * Supports Motorola Binary and NMEA output
  * does not have 100 Hz output
  * does not have TRAIM (Timing Receiver Autonomous Integrity Monitor)
  * does not have sawtooth correction output
  * 1 PPS 500 ns timing
 
  crystal nearest MMCX antenna connector is two-lead can style with bent

  leads for surface mounting
  example p/n label: P183T12N12   (final N = Navigation?)
 
  photos:
  http://www.wa5rrn.com/GPS%20Other/Motorola%20M12/m12.pdf
  https://picasaweb.google.com/bealevideo/GPS#5580118907079326290
 
  Motorola Oncore M12+T Timing GPS:
  ---
  * Supports Motorola Binary output only
  * 1 Hz or 100 Hz output selectable
  * TRAIM (Timing Receiver Autonomous Integrity Monitor)
  * sawtooth correction (clock granularity) message available
  * 1 pps 2nS 1 Sigma, 6nS 6 Sigma (using sawtooth correction message)
  * 1 pps 10nS 1 Sigma, 20nS 6 Sigma (without correction)
 
  smaller leadless surface-mount crystals
  example p/n label: P283T12T17(final T = Timing?)
 
  photos:
  http://www.wa5rrn.com/GPS%20Other/Motorola%20M12/m12plusbrochure.pdf
  http://cgi.ebay.co.uk/ws/eBayISAPI.dll?VISuperSizeitem=290308535362
 
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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Sanjeev Gupta
On Wed, Mar 9, 2011 at 22:09, jimlux jim...@earthlink.net wrote:

 OTOH, if you're building a rocket that's big enough to need something like
 this, you can likely get the needed export licenses, or at least, comply
 with the export control laws.

Wait, he _is_ exporting the whole rocket, anyway, isn't he?

Can you claim a rocket launch as an Export Credit?  Yes, Officer, we
will report to the Customs Department if this equipment re-enters US
Territory.  We will keep track of it, thank you.  And believe me, I
will know _precisely_ when that happens.

--
Sanjeev Gupta
+65 98551208 http://www.linkedin.com/in/ghane

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Chris Albertson
On Wed, Mar 9, 2011 at 5:43 PM, Sanjeev Gupta gha...@gmail.com wrote:

 Can you claim a rocket launch as an Export Credit?  Yes, Officer, we
 will report to the Customs Department if this equipment re-enters US
 Territory.  We will keep track of it, thank you.  And believe me, I
 will know _precisely_ when that happens.

There is precedent  for this in the US.  I know a case where we paid
import duty on an expensive part and then applied for refund and were
granted the refund of duty after launch because the part was
re-exported.   I forget the exact technicalities but the US customs
people treated the item as being imported only for re-shipment outside
the US.

Here is another also from US Customs (My all time favorite bit of bureaucracy)
http://i.space.com/images/i/4460/i02/Apollo-11-Immigration-02.jpg

Another well known case was the optical window used on a Pioneer Venus
spacecraft.  It was cut from a rather large diamond imported from
Europe.  As above import duty was refunded.  This made the news
because of the huge cost of the 3/4 inch diameter diamond they sliced
the window from.




-- 
=
Chris Albertson
Redondo Beach, California

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread jimlux

On 3/9/11 5:43 PM, Sanjeev Gupta wrote:

On Wed, Mar 9, 2011 at 22:09, jimluxjim...@earthlink.net  wrote:


OTOH, if you're building a rocket that's big enough to need something like
this, you can likely get the needed export licenses, or at least, comply
with the export control laws.


Wait, he _is_ exporting the whole rocket, anyway, isn't he?

Can you claim a rocket launch as an Export Credit?  Yes, Officer, we
will report to the Customs Department if this equipment re-enters US
Territory.  We will keep track of it, thank you.  And believe me, I
will know _precisely_ when that happens.



You may laugh, but such questions *do* come up.

And accountants ask where things are..I see you received a GPS receiver 
2 years ago, and I don't see a shipper for it leaving.  Can you tell me 
where it is?


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Re: [time-nuts] GPS Usage

2011-03-09 Thread David I. Emery
On Wed, Mar 09, 2011 at 08:01:31AM +, Poul-Henning Kamp wrote:
 Well, how can you argue with closing a system that was aiding terrorists ?
 
 The reason LORAN-C got killed was that DoD/DHS couldn't jam it if a
 terrorist with a suitcase-nuke was trying to find his way to Congress.

Is this tongue in cheek, or do you have any actual basis
for stating that DHS was afraid Loran C WASN'T jammable ?

If the later, this is a rather provocative concept... make an
increasingly vital but easily jammed resource the only readily available
means of precision position and time determination so the government (or
some government, or for that matter many private malefactors) can be
sure to be able to reliably deny accurate position and or time to the
public (or  at least many targeted groups within  the public) at will ?

I wonder what the threat analysis behind this one was... making
an increasingly vital service more fragile because of what some have
called movie thriller plots ?

Have they really convinced themselves that bad guys CANNOT
figure out a workaround ?   It has always happened in the past...

 
 Your government money at work...


-- 
  Dave Emery N1PRE/AE, d...@dieconsulting.com  DIE Consulting, Weston, Mass 
02493
An empty zombie mind with a forlorn barely readable weatherbeaten
'For Rent' sign still vainly flapping outside on the weed encrusted pole - in 
celebration of what could have been, but wasn't and is not to be now either.


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Re: [time-nuts] GPS Usage

2011-03-09 Thread gary
A good thing every air force base doesn't have a homing beacon. Oh wait, 
never mind.


On 3/9/2011 10:54 PM, David I. Emery wrote:

On Wed, Mar 09, 2011 at 08:01:31AM +, Poul-Henning Kamp wrote:

Well, how can you argue with closing a system that was aiding terrorists ?


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Re: [time-nuts] GPS Usage

2011-03-09 Thread Poul-Henning Kamp
In message 20110310065452.ge6...@pig.dieconsulting.com, David I. Emery writ
es:

 The reason LORAN-C got killed was that DoD/DHS couldn't jam it if a
 terrorist with a suitcase-nuke was trying to find his way to Congress.

   Is this tongue in cheek, or do you have any actual basis
for stating that DHS was afraid Loran C WASN'T jammable ?

I have this information from several independent sources.

   I wonder what the threat analysis behind this one was... making
an increasingly vital service more fragile because of what some have
called movie thriller plots ?

We are talking about DHS, the same people who want to see your junk
in airports, what makes you think there is an analysis and not just
security-theater involved ?

Poul-Henning

-- 
Poul-Henning Kamp   | UNIX since Zilog Zeus 3.20
p...@freebsd.org | TCP/IP since RFC 956
FreeBSD committer   | BSD since 4.3-tahoe
Never attribute to malice what can adequately be explained by incompetence.

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Re: [time-nuts] Spacecraft Timekeeping

2011-03-09 Thread Javier Herrero



El 10/03/2011 02:43, Sanjeev Gupta escribió:

On Wed, Mar 9, 2011 at 22:09, jimluxjim...@earthlink.net  wrote:


OTOH, if you're building a rocket that's big enough to need something like
this, you can likely get the needed export licenses, or at least, comply
with the export control laws.


Wait, he _is_ exporting the whole rocket, anyway, isn't he?

Can you claim a rocket launch as an Export Credit?  Yes, Officer, we
will report to the Customs Department if this equipment re-enters US
Territory.  We will keep track of it, thank you.  And believe me, I
will know _precisely_ when that happens.



It is more a matter about that the involved technology could be ITAR 
classified or with other export restrictions. Ask Hughes and Boeing 
about the fine for export control violations in Intelsat 708 :) 
http://en.wikipedia.org/wiki/Intelsat_708


Regards,

Javier

--

Javier HerreroEMAIL: jherr...@hvsistemas.com
Chief Technology Officer
HV Sistemas S.L.  PHONE: +34 949 336 806
Los Charcones, 17 FAX:   +34 949 336 792
19170 El Casar - Guadalajara - Spain  WEB: http://www.hvsistemas.com


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