Re: [time-nuts] Cutler NAA on 24.0kHz....

2014-08-18 Thread Paul Davis
Nat Semi App Note 72 page 18, par. 6.4 shows the configuration for bandpass 
active filter.  This matches the last LM3900 stage, so you would seem to be 
correct.  The shift in filter frequency for 200bps is because the higher 
modulation rate results in a greater frequency shift. It's like 50hz instead of 
the 25hz of the 100bps rate.

Paul

On Aug 17, 2014, at 4:35 PM, Robert LaJeunesse lajeune...@mail.com wrote:

It's simple, but not obvious. The LM3900 is a Norton amplifier, and while it 
has differential inputs they are current driven. (Most older op amps are 
voltage driven.) The LM3900 is powered from 10V, so I think of that as just 
above the maximimum output voltage. Both the upper amplifier and the second 
lower amplifier have 1M feedback resistors, and + inputs fed 10V by 1M bias 
resistors. That would bias the output at near the supply rail, turning these 
stages into something like half-wave rectifiers. Since the first lower stage 
has a 2M bias resistor it idles at about half supply, and behaves as a simple 
inverter. If my analysis is correct (and I worked at National when the LM3900 
came out, a friend did apps for this odd new part) then the combining of the 
two outputs produces a negative going full wave rectification of the signal. 
The fourth LM3900 stage looks like an inverting bandpass filter, but I'd have 
to dig out some reference books to determine its behavior in more detail. As f
 or the 100-200 switch I'm confused, why would the bandpass frequency be 
lowered for the higher modulation rate?
 
Bob LaJeunesse
 

Sent: Saturday, August 16, 2014 at 2:56 PM
From: Kenneth G. Gordon kgordon2...@frontier.com
To: paul swed paulsw...@gmail.com
Cc: time-nuts@febo.com
Subject: Re: [time-nuts] Cutler NAA on 24.0kHz
On 16 Aug 2014 at 13:35, paul swed wrote:

 
 Kenneth on the opamps that is correct.
 But I put little U's to indicate phase. They actually represent the top half 
 of
 the input cycle.

Yes, I saw those, but unless I am mistaken, you didn't add a U after the
second opamp, which would have returned the phase to the input's.

 In the top path it inverts once.

I see twice: once through the first op amp and again through the second one.
The second one then outputs to the IF.

Anyway, to me, it is a very interesting and simple circuit.

I LIKE simple. I am a great believer in the KISS principle.

Ken W7EKB
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[time-nuts] Mc Coy OCXO in HP equipment.

2014-08-18 Thread EWKehren
I am presently downsizing and that has also resulted in shrinking my HP 70  
000 series spectrum analyzer. Out with the 70310A OCXO reference. The unit 
has a  McCoy OSC92-13B OCXO. The original price was $ 5000 and the option 
with out OCXO  was a $ 2500 saving. Some OCXO. Does any one have any 
information on the unit  and is it used in other equipment. 
Thank you   Bert Kehren
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Re: [time-nuts] Cutler NAA on 24.0kHz....

2014-08-18 Thread paul swed
I may build up the d-msk-r tracor circuit.

I seriously speculate it works as follows.
Tracor down converts NAA's signal to a 100 Hz IF.
The NAA signal is plus and minus 50 Hz msk or FSK
Making the mark 50 Hz and space 150 Hz. (Really don't know whats mark or
space nor does it matter)

The tracor d-msk-r acts as a doubler so 50 Hz becomes 100 Hz only for the
mark condition. The space goes to 300 Hz and the last stage bandpass filter
only passes the doubled mark signal at 100 Hz the signal that the Tracor
can lock to.
I believe the 300 Hz simply leaves gaps in the signal.
Purest of a guess.
When I looked at NAA in spectrum lab it did not appear as a traditional FSK
signal. Instead it was a clearly random signal without clearly defined mark
and space carriers. Kind of pointing to a OPSK like signal.

If the theory is true the d-msk-r only works on an IF of 100 Hz. The reason
tracor selected this IF over the others that could have been used.
Regards
Paul
WB8TSL








On Mon, Aug 18, 2014 at 11:17 AM, Paul Davis 
ziggy9+time-n...@pumpkinbrook.com wrote:

 Nat Semi App Note 72 page 18, par. 6.4 shows the configuration for
 bandpass active filter.  This matches the last LM3900 stage, so you would
 seem to be correct.  The shift in filter frequency for 200bps is because
 the higher modulation rate results in a greater frequency shift. It's like
 50hz instead of the 25hz of the 100bps rate.

 Paul

 On Aug 17, 2014, at 4:35 PM, Robert LaJeunesse lajeune...@mail.com
 wrote:

 It's simple, but not obvious. The LM3900 is a Norton amplifier, and while
 it has differential inputs they are current driven. (Most older op amps are
 voltage driven.) The LM3900 is powered from 10V, so I think of that as just
 above the maximimum output voltage. Both the upper amplifier and the second
 lower amplifier have 1M feedback resistors, and + inputs fed 10V by 1M bias
 resistors. That would bias the output at near the supply rail, turning
 these stages into something like half-wave rectifiers. Since the first
 lower stage has a 2M bias resistor it idles at about half supply, and
 behaves as a simple inverter. If my analysis is correct (and I worked at
 National when the LM3900 came out, a friend did apps for this odd new part)
 then the combining of the two outputs produces a negative going full wave
 rectification of the signal. The fourth LM3900 stage looks like an
 inverting bandpass filter, but I'd have to dig out some reference books to
 determine its behavior in more detail. As f
  or the 100-200 switch I'm confused, why would the bandpass frequency be
 lowered for the higher modulation rate?

 Bob LaJeunesse


 Sent: Saturday, August 16, 2014 at 2:56 PM
 From: Kenneth G. Gordon kgordon2...@frontier.com
 To: paul swed paulsw...@gmail.com
 Cc: time-nuts@febo.com
 Subject: Re: [time-nuts] Cutler NAA on 24.0kHz
 On 16 Aug 2014 at 13:35, paul swed wrote:

 
  Kenneth on the opamps that is correct.
  But I put little U's to indicate phase. They actually represent the top
 half of
  the input cycle.

 Yes, I saw those, but unless I am mistaken, you didn't add a U after the
 second opamp, which would have returned the phase to the input's.

  In the top path it inverts once.

 I see twice: once through the first op amp and again through the second
 one.
 The second one then outputs to the IF.

 Anyway, to me, it is a very interesting and simple circuit.

 I LIKE simple. I am a great believer in the KISS principle.

 Ken W7EKB
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Re: [time-nuts] Cutler NAA on 24.0kHz....

2014-08-18 Thread Charles Steinmetz

Paul wrote:

Nat Semi App Note 72 page 18, par. 6.4 shows the configuration for 
bandpass active filter.  This matches the last LM3900 stage, so you 
would seem to be correct.  The shift in filter frequency for 200bps 
is because the higher modulation rate results in a greater frequency 
shift. It's like 50hz instead of the 25hz of the 100bps rate.


Robert wrote:

It's simple, but not obvious. The LM3900 is a Norton amplifier, and 
while it has differential inputs they are current 
driven.   *  *  *   Both the upper amplifier and the second lower 
amplifier have 1M feedback resistors, and + inputs fed 10V by 1M 
bias resistors. That would bias the output at near the supply rail, 
turning these stages into something like half-wave rectifiers. 
Since the first lower stage has a 2M bias resistor it idles at 
about half supply, and behaves as a simple 
inverter.   *  *  *  combining the two outputs produces a negative 
going full wave rectification of the signal. The fourth LM3900 
stage looks like an inverting bandpass filter, but I'd have to dig 
out some reference books to determine its behavior in more detail. 
As f or the 100-200 switch I'm confused, why would the bandpass 
frequency be lowered for the higher modulation rate?


The circuit as a whole operates as a frequency doubler using 
full-wave rectification and filtering.  The rx LO is 100Hz below the 
nominal carrier frequency, so in normal (non-MSK) mode, the IF 
frequency is 100Hz.  Referring to the MSK addendum, a received 200 
baud MSK signal is 50Hz below nominal, and a 100 baud MSK signal is 
25Hz below nominal.  With the LO 100 Hz below nominal, this makes the 
IF frequency 50Hz when receiving a 200 baud MSK signal, and 75 Hz 
when receiving a 100 baud MSK signal.  After doubling, these become 
100 Hz (200 baud) and 150 Hz (100 baud), so the BPF is switchable 
between 100Hz and 150Hz.  They used a FET to chop the 150Hz (100 
baud) signal with a 50Hz square wave.


I can't say I'm impressed with the design, even for the era.  The 
whole instrument is built mostly with LM3900s, which makes it 
thousands (maybe even millions) of times noisier than it would be if 
it had been properly designed with standard op-amps.  It may work 
more or less, but it's a fugly way to get there.  There are other 
questionable choices (like the FET chopper, an overall design that 
depends on lots of one-shots, etc.).  The designers knew about the 
LM301 (there is one in the unit), so there was really no excuse for 
using LM3900s.  Yeah, the 301 was more expensive -- but this was 
supposed to be a state-of-the-art measuring device for characterizing 
good OCXOs down to PPB or below.


I simulated the MSK board in LTspice.  Let me know (OFFLIST ONLY, 
please) if you would like the files to play with (662kB ZIP 
file).  (Note that these won't do you any good if you're not an 
LTspice user.)  Again, please do not clutter the list with requests 
for files -- OFFLIST ONLY, please (check your headers carefully 
before you hit Send).


Best regards,

Charles



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[time-nuts] MH370 Doppler

2014-08-18 Thread Joe Leikhim
Is anyone paying attention to all the chatter about the lost aircraft 
MH370, Inmarsat's supposed flight tracks based on 6 or 7 pings (1 per 
hour), the Doppler shift (BFO) and transaction timing (BTO) etc??


Basically from my perspective they are putting too much stock into the 
Doppler which relies in part upon the stability of the satellite 
terminal in the 777 aircraft. My question is how stable an oscillator 
(reported OCXO - not confirmed)  would be under the extremes of either 
or both a cabin fire or decompression event. There is a website (Duncan 
Steel Blog) where some math brains are trying to sort out the raw data 
provided by Inmarsat. They have made assumptions about the stability of 
the local oscillator in the satellite, but I think the aircraft 
satellite terminal's master oscillator is a variable they have pushed 
aside.


--
Joe Leikhim


Leikhim and Associates

Communications Consultants

Oviedo, Florida

jleik...@leikhim.com

407-982-0446

WWW.LEIKHIM.COM

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Re: [time-nuts] MH370 Doppler

2014-08-18 Thread Brian, WA1ZMS
I thought that Inmarsat terminals had AFC to the sat's down-link.  Not to the 
degree of true phase-lock like DSN has but enough so that the sat's abillity to 
do doppler correction on the uplink is valid to help with BER, etc... Otherwise 
the doppler correction would be of no help and not be needed.

-Brian, WA1ZMS/4
iPhone

 On Aug 18, 2014, at 12:53 PM, Joe Leikhim jleik...@leikhim.com wrote:
 
 Is anyone paying attention to all the chatter about the lost aircraft MH370, 
 Inmarsat's supposed flight tracks based on 6 or 7 pings (1 per hour), the 
 Doppler shift (BFO) and transaction timing (BTO) etc??
 
 Basically from my perspective they are putting too much stock into the 
 Doppler which relies in part upon the stability of the satellite terminal in 
 the 777 aircraft. My question is how stable an oscillator (reported OCXO - 
 not confirmed)  would be under the extremes of either or both a cabin fire or 
 decompression event. There is a website (Duncan Steel Blog) where some math 
 brains are trying to sort out the raw data provided by Inmarsat. They have 
 made assumptions about the stability of the local oscillator in the 
 satellite, but I think the aircraft satellite terminal's master oscillator is 
 a variable they have pushed aside.
 
 -- 
 Joe Leikhim
 
 
 Leikhim and Associates
 
 Communications Consultants
 
 Oviedo, Florida
 
 jleik...@leikhim.com
 
 407-982-0446
 
 WWW.LEIKHIM.COM
 
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[time-nuts] Fwd: Re: Fwd: MH370 Doppler

2014-08-18 Thread Joe Leikhim


Because of the bent pipe transponder there is a doppler shift on the 
uplink from the terminal in the aircraft and doppler on the downlink 
from the satellite. Each has to be calculated differently because of the 
relative motion of the satellite (to ground station and aircraft) and 
the gross difference in UL and DL frequency bands.


The local oscillator in the satellite is subject to drift due to solar 
temperature changes as the satellite drifts in and out of eclipse. This 
is apparently being considered.


However, the Doppler parameter called burst frequency offset is a 
value reported by the satellite terminal to the ground station.


My point is that, all of the discussion I have read ignores the 
possibility that the master oscillator aboard the aircraft is also 
subjsect to drift due to thermal effects and those effects could be 
quite significant if a fire on board. . Remember this Doppler shift is 
not being tracked (observed) continuously, rather as a periodic data 
point reported from the aircraft terminal on hourly intervals. Not like 
averaging the tone from a train whistle to get a baseline.




On 8/18/2014 4:13 PM, Brian, WA1ZMS wrote:

Joe-

My understanding is that the Inmarsat link has doppler correction as 
one of the parameters that the bird calculates from each ping heard. 
So it matters not much if the LO on the sat drifts. So long as you 
have the previous data you can plot a trend line. The trend is the sat 
LO drift and the delta from that trend is the dopler.


 At least that's how I read the raw Inmarsat data.  I may be wrong. 
Need to think about it more.


-Brian, WA1ZMS/4
iPhone

Begin forwarded message:


*From:* Joe Leikhim jleik...@leikhim.com mailto:jleik...@leikhim.com
*Date:* August 18, 2014 at 12:53:24 PM EDT
*To:* time-nuts@febo.com mailto:time-nuts@febo.com
*Subject:* *[time-nuts] MH370 Doppler*
*Reply-To:* Discussion of precise time and frequency measurement 
time-nuts@febo.com mailto:time-nuts@febo.com


Is anyone paying attention to all the chatter about the lost aircraft 
MH370, Inmarsat's supposed flight tracks based on 6 or 7 pings (1 per 
hour), the Doppler shift (BFO) and transaction timing (BTO) etc??


Basically from my perspective they are putting too much stock into 
the Doppler which relies in part upon the stability of the satellite 
terminal in the 777 aircraft. My question is how stable an oscillator 
(reported OCXO - not confirmed)  would be under the extremes of 
either or both a cabin fire or decompression event. There is a 
website (Duncan Steel Blog) where some math brains are trying to sort 
out the raw data provided by Inmarsat. They have made assumptions 
about the stability of the local oscillator in the satellite, but I 
think the aircraft satellite terminal's master oscillator is a 
variable they have pushed aside.


--
Joe Leikhim


Leikhim and Associates

Communications Consultants

Oviedo, Florida

jleik...@leikhim.com mailto:jleik...@leikhim.com

407-982-0446

WWW.LEIKHIM.COM http://WWW.LEIKHIM.COM

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--
Joe Leikhim


Leikhim and Associates

Communications Consultants

Oviedo, Florida

jleik...@leikhim.com

407-982-0446

WWW.LEIKHIM.COM


--
Joe Leikhim


Leikhim and Associates

Communications Consultants

Oviedo, Florida

jleik...@leikhim.com

407-982-0446

WWW.LEIKHIM.COM



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Re: [time-nuts] Fwd: Re: Fwd: MH370 Doppler

2014-08-18 Thread Poul-Henning Kamp

In message 53f268cf.80...@leikhim.com, Joe Leikhim writes:

My point is that, all of the discussion I have read ignores the 
possibility that [...]

The major point being ignored is that the terminal in the plane
does a signon after approx 45-60 minutes (can't remember exact
duration -- it's in the data released.)

That means that the terminal was powered on.

That implies it was previously powered off.

The terminal doesn't power on by it's on, somebody is in the
plane at that point, messing with circuit breakers.

The hopeful interpretation is that somebody in the cockpit
is heroically fighting to reconfigure the plane so he can
call mayday and/or gain control.

The conspiratorical interpretation is that in the time interval
between the previous ping and the sign on, there plenty of time to
land the plane at some marginally suitable strip, do what what you
came for, take off, reconfigure the plane and autopilot and leave by
parachute via the back door.

The quick detour into the extreme high corner of the planes
envelope which seems perfectly designed to incapacitate the
passengers makes me lean towards the latter.

-- 
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] MH370 Doppler

2014-08-18 Thread David I. Emery
On Mon, Aug 18, 2014 at 04:18:30PM -0400, Brian, WA1ZMS wrote:

 I thought that Inmarsat terminals had AFC to the sat's down-link.  Not
 to the degree of true phase-lock like DSN has but enough so that the
 sat's abillity to do doppler correction on the uplink is valid to help
 with BER, etc... Otherwise the doppler correction would be of no help
 and not be needed.

I beleive most Aero Classic terminals use a fairly good
OCXO.   Somewhere I may have a limit spec on stability, but those
docs are not immediately handy.

Normally a demod in the terminal is kept tuned to one of the
continuous L band control channels which I believe may be Doppler
compensated in the ground uplink transmitter for the 6 Ghz C band uplink
Doppler and LO drift on the satellite so it is correctly on frequency as
radiated on the L band downlink.   This could supply a frequency
reference to the terminal that could be used to AFC the terminal
frequency standard so it is close to right on.   Doing this would
require terminal firmware to determine estimated Doppler at the L band
control channel downlink frequency from the satellite based on some
estimate of the planes position, satellite position and relative
velocities.

The QPSK DSP modems used at both ends would be easily able to
supply estimated frequency offset, both on the ground at ground earth
station and in the plane. It is presumably true that this measurement is
corrected on the ground end for the Doppler due to movement of the
satellite relative to the ground station on the C band downlink relaying
the L band uplinks from the plane so it reflects frequency error as seen
at the satellite on the L band uplink with the downlink and satellite LO
drift terms removed.   I presume this is what INMARSAT is reporting, but
am not sure.

IIRC the plane is expected to adjust its burst uplink frequency
and timing to come out right at the satellite receive antenna... thus 
compensating for the uplink Doppler at L band and the time delay too.
But I do remember that the ground supplies feedback on the control
channel as to how much the plane is off so it can adjust...

Guess it might be time to dig out the docs again.

-- 
  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] Mc Coy OCXO in HP equipment.

2014-08-18 Thread Richard (Rick) Karlquist

I am just speculating that this oscillator was used
instead of the 10811 because the 10811 would not fit.
Therefore, it would NOT be used in other equipment.
I would guess the specs would be similar to the 10811.
The 70,000 series had some general purpose power bus
that the McCoy would have to run off of.  It might
use different voltages than the 10811.

Rick

On 8/18/2014 8:55 AM, ewkeh...@aol.com wrote:

I am presently downsizing and that has also resulted in shrinking my HP 70
000 series spectrum analyzer. Out with the 70310A OCXO reference. The unit
has a  McCoy OSC92-13B OCXO. The original price was $ 5000 and the option
with out OCXO  was a $ 2500 saving. Some OCXO. Does any one have any
information on the unit  and is it used in other equipment.
Thank you   Bert Kehren
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Re: [time-nuts] DIY FE-5680A lobotomy (disable temp compensation)

2014-08-18 Thread Angus
On Fri, 04 Jul 2014 02:35:41 +0100, you wrote:


Hi Bert,

I am thinking about testing a heat pipe on a fan cooled setup I use.
The first temp controlled chassis I did used a peltier and works very
well, but was a lot more work to do and is much more power hungry. 

The main problem I find is not the temp controller itself, but rather
the change in the temperature across the chassis as the ambient
changes. However good the temp controller is, it only controls a
single point, but other points further away from the sensing
thermistor can vary a lot. 
I noticed you posted a picture of a heat pipe cooler a couple of weeks
ago - did you happen to compare the temperature across the unit with
direct fan cooling and the heat pipe cooler, or with different heat
pipes?

Angus.


I finally got around to playing with a couple of laptop heat pipes,
fixed to a 25x50x75mm block of aluminium which is fixed to the 12mm
thick baseplate. 
On a quick test of it, a sensor near the end of the baseplate showed
1.5-2x greater variation with temperature compared with just having a
fan blow directly onto the baseplate. 
The oscillator also had to be allowed to run a few degrees C hotter
for the heatpipe coolers to work to the same max ambient temp.

One cooler had two heatpipes with about 12cm between the aluminium
block and the heatsink fins (cast in this case) The other had a
single, wider heat pipe with about 5cm between the block and the
heatsink (this time with a lot more fine fins) 

The second cooler was rather more efficient, allowing a extra degreee
of cooling at the top end, but more problematic was that it entered
'bang-bang' mode with the analogue temperature controller even sooner,
and the temperature fluctuations there were greater. Both were rather
worse than with the fan just blowing onto the baseplate.

Using a PWM fan controller would help a good bit, but getting more
creative with a microcontroller would be better. That way you can give
the fan a minimum of a small kick every so often, and vary the
repetition rate as well as the duty cycle as more cooling is needed.
With feedback from the fan and even air temperature monitoring, you
could get a good idea of exactly how much cooling was being applied.

Another problem is that the overall temp control range is lower with
the coolers - barely 8-9 DegC compared with 12+ DegC with the fan
blowing directly on the baseplate. That's mainly the result of the
poorer cooling at the top end of the range.

The Rb osc fitted during this test was a SA.22c which takes a good bit
less power than a 5680A, and the fan blowing onto the baseplate was
normally a 60mm one fitted about 50mm away from it. The baseplate was
horizontal with the fan blowing onto it from below.

Maybe fitting a heatsink directly onto the base would help further
with the maximum temp, but it would increase the convection cooling at
the minimum temp, reducing the overall benefit. It could also be more
susceptible to drafts, and would make the fan control much more
delicate.

Anyway, that's the results I got with my setup. Other setups and more
fine tuning could change things a good bit, but I just wanted to get
an idea of how the two cooling methods compared on the same setup.

Angus



On Sat, 28 Jun 2014 12:37:37 -0400 (EDT), you wrote:

Will someone beside us use heat pipe. Would love to have an impendent  
input. What does it take to get a test going. Scott has done a lot of work, 
how  
about some one else step up to the plate. There are a lot of time nuts out 
there  with the 5680A,many for the first time will have a very good 
reference and some  of our experts with proper equipment can make a big 
difference.
Bert Kehren
 
 
In a message dated 6/28/2014 12:20:12 P.M. Eastern Daylight Time,  
newell+timen...@n5tnl.com writes:

At 04:32  AM 6/28/2014, wb6bnq wrote:

monitoring process ?  In other  words have you traced out the 
connections to see what is driving the  pin you think is the temperature 
input ?

No. I've only traced back from  the ADC input to the voltage divider.


The next big question is  have you monitored the frequency and its 
stability, externally, to  observe what effects are taking place when 
you disable this input to  the A/D ?

I have not.


That sounds complicated and messy  but may be easier than it 
appears.  An appropriate container  would be:

It does sound messy. I don't think I'm willing to dunk one of  my units.
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