[amsat-bb] Re: Antenna Polarization

2009-05-25 Thread k9qho6762
This is what I would recommend.
 
I do not have polarization switching for either of my antennas.
 
My 11 turn helix on 435 MHz is RHCP
 
My 14 element KLM on 144 MHz is LHCP
 
K9CIS has studied the polarizations of the uplink/downlink signals from AO-7, 
VO-52, and FO-29 and this seems to be the best selection.
 
Using his recommendation, I do remember switching my KLM from RH to LH because 
AO7's downlink was weak and switching did solve the problem.
 
The helix (polarization cannot be switched) was constructed for AO-40 (which 
was RH) and easily hears FO-29.
 
The optimum set-up is to be able to switch polarization, but you know how 
things go in the world of ham radio.
 
All the best.
 
Mike (K9QHO)
AMSAT 33589
 
 
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[amsat-bb] Re: Antenna Polarization

2009-09-25 Thread i8cvs
- Original Message - 
From: "Patrick Domack" 
To: 
Sent: Wednesday, September 23, 2009 4:11 AM
Subject: [amsat-bb] Antenna Polarization

> I've been meaning to setup some antennas for satellite operation for  
> awhile here. And since I will probably end up doing it this  
> fall/winder I had a question I was wondering about, before I get the  
> antennas completely built connected up.
> 
> I plan on using a circular polarized antenna, for lhcr and rhcr.
> Since this setup has two coax that your switch a 1/4wave (if I  
> remember right) to either side to create the two rotations in the  
> antenna.
> 
> Is there a way I can modify this to feed two radios? so one radio  
> would receive lhcr, and the other rhcr? Or would I be forced to use  
> two antennas to do this?
> 
> The only idea I have is to use a signal splitter on each of the two  
> antenna halfs before joining them, then join each of those splits into  
> the cr parts. But I'm not sure if there is a better way to do this  
> without as much loss, or if this might cause a backfeed that would  
> defeat the me from getting any signal at all.
> 
> Maybe there is a good writeup of this on the web somewhere, but I have  
> no clue what the proper terms to google it are, and haven't had any  
> luck.
> 
> Thanks.
> 
Hi Patrick

What you propose to do is possible in theory but you need four 3 dB 
power dividers with characteristic impedance of 36 ohm each and 14
N/m male connectors so that the total losses of the system are too high.
I suggest to switch from RHCP to LHCP over the same receiver using
only a coax relay as described in all antenna books of the ARRL or into
"The Satellite Experimenter's Handbook by Martin Davidoff K2UBC
edited by the ARRL 

73" de
i8CVS Domenico 



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[amsat-bb] Re: Antenna Polarization Question

2012-09-15 Thread Jim Jerzycke

I run linear polarization, and just live with the fades.

Saves a lot of complexity and headaches!

73, Jim  KQ6EA

On 09/15/2012 06:47 PM, Thomas Doyle wrote:

I was listening to a couple of guys on FO-29 having a nice chat about
satellite antenna polarization. They were trying to figure out what
type of polarization FO-29 used. They looked at the picture of FO-29
on the AMSAT web site and decided that it was not circular. Someone
told me that it was circular so I started looking for information.
Found this page by WD0E which is quite nice.

http://www.amsat.org/amsat-new/information/faqs/pswitch.php

Is there a more current page that contains this type of information.

tnx W9KE Tom Doyle
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[amsat-bb] Re: Antenna Polarization Question

2012-09-15 Thread i8cvs
- Original Message -
From: "Thomas Doyle" 
To: 
Sent: Saturday, September 15, 2012 8:47 PM
Subject: [amsat-bb] Antenna Polarization Question

> I was listening to a couple of guys on FO-29 having a nice chat about
> satellite antenna polarization. They were trying to figure out what
> type of polarization FO-29 used. They looked at the picture of FO-29
> on the AMSAT web site and decided that it was not circular. Someone
> told me that it was circular so I started looking for information.
> Found this page by WD0E which is quite nice.
>
> http://www.amsat.org/amsat-new/information/faqs/pswitch.php
>
> Is there a more current page that contains this type of information.
>
> tnx W9KE Tom Doyle

Hi Tom, W9KE

For the antenna polarization of FO-29 please read belove:
---
AMSAT NEWS SERVICE BULLETIN 254.S1
FROM AMSAT HQ SILVER SPRING, MD, September 10, 2012
TO ALL RADIO AMATEURS
BID: $WSR-254.S1

FO-29 JAS-2
Catalog number: 24278
Launch Date: August 17, 1996

Mode and Antenna Polarization:
V: RHCP
U: RHCP

i8CVS Note:

Following my experience on FO-29 I can add the information
belowe:

FO-29 is RHCP circularly polarized  both in uplink and downlink
and has a fixed sense both up and down, but because of its orbit 
geometry and motion, continuously good signals through it for an
entire pass can only maintained if the antennas ground station sense
is switched, RHCP to LHCP and vice versa in 70 cm and 2 meters
usually several times and on both uplink and downlink and so 
polarization switching relays on board of both up and down antennas
are recommended. 

Read please my articles about polarization switching published on
the AMSAT-Journal March/April 2007 and May/June 2007  

73" de

i8CVS Domenico

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[amsat-bb] Re: Antenna Polarization Question

2012-09-15 Thread Thomas Doyle
Domenico,

Thanks for the reply. I am slowly building my sat station back to what
it was back in the day when I had a pair of KLM antennas with
polarization switching. I have recently added a switchable
polarization 70 cm antenna to my current station and am amazed at how
often during an FO-29 pass it is necessary to change polarization. My
memory is not what it should be but I do not remember as much
switching being necessary when using AO-10 era sats. Perhaps they were
more stable or the pass was so long that it did not seem like it
required as much switching.

 "In 1911, Albert Abraham Michelson discovered that light reflected
from the golden scarab beetle Chrysina resplendens is preferentially
left-handed." After reading this I wondered if it is possible to
create a reflector for RF that would do something similar to what this
tiny insect does without even trying. When I asked how to change the
polarization sense of a lindenblad antenna I was going to build the
author of the article told me that it was not necessary to switch it
because there were so many reflections it would not matter. Perhaps a
controlled reflective surface would work.

tnx & 73 W9KE Tom Doyle



On Sat, Sep 15, 2012 at 3:00 PM, i8cvs  wrote:
> - Original Message -
> From: "Thomas Doyle" 
> To: 
> Sent: Saturday, September 15, 2012 8:47 PM
> Subject: [amsat-bb] Antenna Polarization Question
>
>> I was listening to a couple of guys on FO-29 having a nice chat about
>> satellite antenna polarization. They were trying to figure out what
>> type of polarization FO-29 used. They looked at the picture of FO-29
>> on the AMSAT web site and decided that it was not circular. Someone
>> told me that it was circular so I started looking for information.
>> Found this page by WD0E which is quite nice.
>>
>> http://www.amsat.org/amsat-new/information/faqs/pswitch.php
>>
>> Is there a more current page that contains this type of information.
>>
>> tnx W9KE Tom Doyle
>
> Hi Tom, W9KE
>
> For the antenna polarization of FO-29 please read belove:
> ---
> AMSAT NEWS SERVICE BULLETIN 254.S1
> FROM AMSAT HQ SILVER SPRING, MD, September 10, 2012
> TO ALL RADIO AMATEURS
> BID: $WSR-254.S1
>
> FO-29 JAS-2
> Catalog number: 24278
> Launch Date: August 17, 1996
>
> Mode and Antenna Polarization:
> V: RHCP
> U: RHCP
> 
> i8CVS Note:
>
> Following my experience on FO-29 I can add the information
> belowe:
>
> FO-29 is RHCP circularly polarized  both in uplink and downlink
> and has a fixed sense both up and down, but because of its orbit
> geometry and motion, continuously good signals through it for an
> entire pass can only maintained if the antennas ground station sense
> is switched, RHCP to LHCP and vice versa in 70 cm and 2 meters
> usually several times and on both uplink and downlink and so
> polarization switching relays on board of both up and down antennas
> are recommended.
>
> Read please my articles about polarization switching published on
> the AMSAT-Journal March/April 2007 and May/June 2007
>
> 73" de
>
> i8CVS Domenico
>



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[amsat-bb] Re: Antenna Polarization Question

2012-09-15 Thread i8cvs
- Original Message - 
From: "Thomas Doyle" 
To: "i8cvs" 
Cc: "Amsat - BBs" 
Sent: Saturday, September 15, 2012 10:34 PM
Subject: Re: [amsat-bb] Antenna Polarization Question

> Domenico,
> 
> Thanks for the reply. I am slowly building my sat station back to what
> it was back in the day when I had a pair of KLM antennas with
> polarization switching. I have recently added a switchable
> polarization 70 cm antenna to my current station and am amazed at how
> often during an FO-29 pass it is necessary to change polarization. My
> memory is not what it should be but I do not remember as much
> switching being necessary when using AO-10 era sats. Perhaps they were
> more stable or the pass was so long that it did not seem like it
> required as much switching.
>
< snip >
> 
> tnx & 73 W9KE Tom Doyle
> 
Hi Tom, W9KE

Using AO-10 and in general HEO satellites like AO-13 and AO40
switching polarization was less necessary than using LEO satellites 
because most of the time the satellite antennas were oriented toward
the earth with a small squint angle so that the polarization changed
very slowly mostly due only to the Faraday polarization rotation
when the wave passed through the ionosphere.

BTW the above HEO satellites were spinning over the Z axis 
generating the so called "spin modulation" wich sounded like
WOW...WOW.WOW.WOW

Only the AO40 downlink at 2401 MHz was less affected by the
polarization rotation due to Faraday effect and less affected by 
the spin modulation.

Hope that some time in the future the HEO satellite P3E will
be placed in orbit !

73" de 

i8CVS Domenico
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Thomas Doyle
Andy,

I believe that is true but that does not explain why the optimum
polarity setting on the receive end would
change during a pass. Perhaps there is some sort of Faraday Rotation
effect but I do not believe that
it can change the direction of the circular polarized signal but who
knows what magic things happen in
the ether.

tnx & 73 W9KE Tom Doyle


On Sat, Aug 4, 2012 at 12:44 PM, andrew abken  wrote:
>
> Hi Tom,
>
>I thought fo-29 was transmitting circular. Would not surprise me if I was 
> wrong:)
>
>   Andy,
>kn6za
>
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tom ...
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread andrew abken



  Hi Tom,

   I have also noticed the switching of polarity as the sat travels over.

   What I have understood to be the mode by which this is occuring comes from 
the fact that circular polarized antennas change polarity as you move out of 
the main radiation lobe. The main lobe is circular one direction and the next 
lobe is reversed, and the next reversed back again.

  Hope someone can correct me if I have things fouled up.

   Andy

> Date: Sat, 4 Aug 2012 14:13:47 -0500
> Subject: Re: [amsat-bb] Antenna Polarization Technical Question
> From: tomdoyle1...@gmail.com
> To: kn...@hotmail.com
> CC: amsat-bb@amsat.org
> 
> Andy,
> 
> I believe that is true but that does not explain why the optimum
> polarity setting on the receive end would
> change during a pass. Perhaps there is some sort of Faraday Rotation
> effect but I do not believe that
> it can change the direction of the circular polarized signal but who
> knows what magic things happen in
> the ether.
> 
> tnx & 73 W9KE Tom Doyle
> 
> 
> On Sat, Aug 4, 2012 at 12:44 PM, andrew abken  wrote:
> >
> > Hi Tom,
> >
> >I thought fo-29 was transmitting circular. Would not surprise me if I 
> > was wrong:)
> >
> >   Andy,
> >kn6za
> >
> > ___
> > Sent via AMSAT-BB@amsat.org. Opinions expressed are those of the author.
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> 
> 
> 
> -- 
> 
> Sent from my computer.
> 
> tom ...
  
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Bob Bruninga
> I believe that is true but that does not explain 
> why the optimum polarity setting on the receive 
> end would change during a pass. 

That's easy.  The circularity on a pair of crossed dipoles (about all  you can 
get on a spacecraft) May be designed for Right hand circularity when viewed 
from the prime direction.  But by definition, that save waveform will be LHC 
when viewed from the opposite direction.

And since the geometry to any one observer is constantly changing by almost 180 
degrees during an overhead pass, that is why it is very easy to see, complete 
change in circularity.

Bob, WB4APR

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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Thomas Doyle
Bob,

Thanks for the reply. A student of mine once told me that if someone
tells you something is easy - it is not. Even though this is not only
easy but "very easy" I still need a slight clarification. I think it
boils down to the orientation of the satellite relative to the center
of the earth.

If the satellite was a clock and the face of the clock was oriented
toward the center of the earth the I believe the clock would appear to
rotate CW on both ends of the pass. If the side of the clock rather
than the face of the clock was oriented toward the center of the earth
it would appear to rotate one way at the start of the pass and the
other way at the end of the pass because we would be looking at the
clock from the other side. I believe this is the basis of the "very
easy" explanation you offered.

Not sure why anyone would want to maintain the orientation of the
satellite in such a way that would cause the direction of circular
polarization to change during the path. Perhaps people selling antenna
circularity switches would like it but other than that I do not
understand why it would be done. I am most likely missing something
important.

tnx & 73 W9KE Tom Doyle




On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
>> I believe that is true but that does not explain
>> why the optimum polarity setting on the receive
>> end would change during a pass.
>
> That's easy.  The circularity on a pair of crossed dipoles (about all  you 
> can get on a spacecraft) May be designed for Right hand circularity when 
> viewed from the prime direction.  But by definition, that save waveform will 
> be LHC when viewed from the opposite direction.
>
> And since the geometry to any one observer is constantly changing by almost 
> 180 degrees during an overhead pass, that is why it is very easy to see, 
> complete change in circularity.
>
> Bob, WB4APR
>



-- 

Sent from my computer.

tom ...

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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Bob DeVarney W1ICW
I can't explain it but have noticed the same polarity changes during a 
pass. Like S-9 to S-1/nothing switching between polarities with my 
antennas... it's been  handy to actually have the ability to change 
polarities in the past for me. I do not have the ability to polarity 
switch on 2 meters, only 70 cM for the downlink.


73,

Bob W1ICW

On 8/4/2012 3:13 PM, Thomas Doyle wrote:

Andy,

I believe that is true but that does not explain why the optimum
polarity setting on the receive end would
change during a pass. Perhaps there is some sort of Faraday Rotation
effect but I do not believe that
it can change the direction of the circular polarized signal but who
knows what magic things happen in
the ether.

tnx & 73 W9KE Tom Doyle


On Sat, Aug 4, 2012 at 12:44 PM, andrew abken  wrote:

Hi Tom,

I thought fo-29 was transmitting circular. Would not surprise me if I was 
wrong:)

   Andy,
kn6za

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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread andrew abken

  Tom,

   I don't think any one who designs a system "wants" this to occur, but as a 
function of overall system cost it is one of the unavoidable realities.

   Its actually a great compromise, because with only a 3db loss you can use a 
linear rec. antenna with no polarity switching, and avoid the large fading that 
would occur if the satellite was transmitting linear.

  Now if you have the money to build a satellite that can point itself at the 
receiving station at all times ie: geo synchronous:) then that would be the 
cats meow;)

  73
  Andy

> Not sure why anyone would want to maintain the orientation of the
> satellite in such a way that would cause the direction of circular
> polarization to change during the path. Perhaps people selling antenna
> circularity switches would like it but other than that I do not
> understand why it would be done. I am most likely missing something
> important.

  
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Stephen Melachrinos
 
> Not sure why anyone would want to maintain the orientation of the
> satellite in such a way that would cause the direction of circular
< polarization to change during the path. 

There are two perspectives in answering this.

1. You used the word "maintain," which implies the ability of the spacecraft to 
control its attitude. That's commonly done for commercial and military 
satellites, but rarely (if ever) done for amateur satellites. It's just too 
complicated and too expensive for amateurs to allocate the resources to make it 
happen.

2. You also asked why anyone would WANT to maintain the orientation like that. 
In a more general sense, recognize that not every satellite is a communications 
satellite, supporting communications with terrestrial stations. Scientific 
missions often have to point a body-mounted sensor somewhere, and the comm 
payload has to "adjust." For example, Hubble's main body IS the telescope, so 
it MUST point at the astronomical targets. For that mission, NASA paid for an 
articulated communications payload, but  spacecraft don't always do that. 

73,
Steve
W3HF
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread Bob Bruninga
> Not sure why anyone would want to maintain the 
> orientation of the satellite in such a way that 
> would cause the direction of circular
> polarization to change during the path. 

Lets try this approach... As I said before,  By the laws of physics, what comes 
out one side of a circular polarized low gain antenna as RHCP comes out the 
opposite side as LHCP.

Now given that, and the fact that someone in Maryland is in the center of the 
RHCP beam, then by the laws of physics, the guy in California must see mostly 
LHCP.  No matter how much one of those persons demands that he deserves the 
RHCP beam, by definition, someone else somewhere will get the LHCP one, and the 
geometry changes at least every 10 minutes or so and every time the spacecraft 
rotates a bit.

So one might say, "point it down" then only the person in Kansas will see the 
main beam and those in CA or MD will be completely off the sides almost 70 
degrees from the main beam.  Mot people do not realize how LOW these satellites 
are.  The only solution is to put satellites so high, that "down" is about the 
same to everyone (geostationary altitude).  But then that takes 100 times more 
altitude, and that takes 10,000 times more power.

Better to just live with the laws of physics... I guess.

Bob, WB4aPR

>
>On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
>>> I believe that is true but that does not explain
>>> why the optimum polarity setting on the receive
>>> end would change during a pass.
>>
>> That's easy.  The circularity on a pair of crossed dipoles (about all  you 
>> can get on a spacecraft) May be designed for Right hand circularity when 
>> viewed from the prime direction.  But by definition, that save waveform will 
>> be LHC when viewed from the opposite direction.
>>
>> And since the geometry to any one observer is constantly changing by almost 
>> 180 degrees during an overhead pass, that is why it is very easy to see, 
>> complete change in circularity.
>>
>> Bob, WB4APR
>>
>
>
>
>-- 
>
>Sent from my computer.
>
>tom ...
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread i8cvs
Hi Thomas, W9KE

In a separate email I have sent to you a very compreensive article
explaining why during an orbit of a LEO satellite like FO-29 the
changes in polarization is generated.

73" de

i8CVS Domenico

- Original Message -
From: "Thomas Doyle" 
To: 
Sent: Saturday, August 04, 2012 4:46 PM
Subject: [amsat-bb] Antenna Polarization Technical Question


> I had a actual qso on FO-29 the other day and during the contact
> circular polarization switching was discussed.
> The station I was talking with described a very large change in
> received signal strength when switching
> between LHCP and RHCP. I have heard other people mention this and I
> recall some change when using
> AO-10 with my switchable KLM's back in the good old days.
>
> I have been trying to figure out why there would be such a big change.
> Here is a collection of theories/questions.
>  I would appreciate comments on any or all of them. This is a bit
> complex so a direct reply is probably best.
>
> - In a perfect world if the satellite antenna is linearly polarized
> LH-RH switching would not make any difference.
>
> - In a real world it is unlikely that the ground station receive
> antenna is truly circular. It is somewhat elliptical.
>
> Question: if the receive antenna has an elliptical pattern does the
> angle of the major axis change when
> switching LH - RH.
> This is  a complex question related to the nature of what caused the
> elliptical distortion in the pattern.
> Perhaps someone has measured this.  If the angle of the major axis
> receive antenna pattern changes when
> switching between LH and RH and the satellite antenna is linearly
> polarized this could account for some change
> in received signal strength. Other than that I am at a loss to explain
> why switching LH-RH on a receive antenna
> would cause a large change in the strength of a signal received from a
> linear antenna.
>
>
> tnx & 73 W9KE Tom Doyle
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread i8cvs
Hi Tom, KN6ZA

With only a 3db loss you can use a linear rec. antenna with no polarity
switching, and avoid the large fading that would occur if the satellite was
transmitting circular RHCP or LHCP(but not linear as you stated)

On the other side if you receive linear and the satellite transmit linearly
with opposite polarity you get more than 20dB of fading.

73" de

i8CVS Domenico

- Original Message -
From: "andrew abken" 
To: ; 
Sent: Saturday, August 04, 2012 10:45 PM
Subject: [amsat-bb] Re: Antenna Polarization Technical Question


>
>   Tom,
>
>I don't think any one who designs a system "wants" this to occur, but
as a function of overall system cost it is one of the unavoidable realities.
>
>Its actually a great compromise, because with only a 3db loss you can
use a linear rec. antenna with no polarity switching, and avoid the large
fading that would occur if the satellite was transmitting linear.
>
>   Now if you have the money to build a satellite that can point itself at
the receiving station at all times ie: geo synchronous:) then that would
be the cats meow;)
>
>   73
>   Andy
>
> > Not sure why anyone would want to maintain the orientation of the
> > satellite in such a way that would cause the direction of circular
> > polarization to change during the path. Perhaps people selling antenna
> > circularity switches would like it but other than that I do not
> > understand why it would be done. I am most likely missing something
> > important.
>
>
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-04 Thread i8cvs
Hi All,

I agree completely with Bob, WB4APR and this is what is wery well
explained into the article "CIRCULAR POLARIZATION by K4KJ,
a zipped file 5 MB long available from me.

73" de

i8CVS Domenico

- Original Message -
From: "Bob Bruninga " 
To: "Thomas Doyle" 
Cc: ; "andrew abken" 
Sent: Sunday, August 05, 2012 12:24 AM
Subject: [amsat-bb] Re: Antenna Polarization Technical Question


> > Not sure why anyone would want to maintain the
> > orientation of the satellite in such a way that
> > would cause the direction of circular
> > polarization to change during the path.
>
> Lets try this approach... As I said before,  By the laws of physics, what
comes out one side of a circular polarized low gain antenna as RHCP comes
out the opposite side as LHCP.
>
> Now given that, and the fact that someone in Maryland is in the center of
the RHCP beam, then by the laws of physics, the guy in California must see
mostly LHCP.  No matter how much one of those persons demands that he
deserves the RHCP beam, by definition, someone else somewhere will get the
LHCP one, and the geometry changes at least every 10 minutes or so and every
time the spacecraft rotates a bit.
>
> So one might say, "point it down" then only the person in Kansas will see
the main beam and those in CA or MD will be completely off the sides almost
70 degrees from the main beam.  Mot people do not realize how LOW these
satellites are.  The only solution is to put satellites so high, that "down"
is about the same to everyone (geostationary altitude).  But then that takes
100 times more altitude, and that takes 10,000 times more power.
>
> Better to just live with the laws of physics... I guess.
>
> Bob, WB4aPR
>
> >
> >On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
> >>> I believe that is true but that does not explain
> >>> why the optimum polarity setting on the receive
> >>> end would change during a pass.
> >>
> >> That's easy.  The circularity on a pair of crossed dipoles (about all
you can get on a spacecraft) May be designed for Right hand circularity when
viewed from the prime direction.  But by definition, that save waveform will
be LHC when viewed from the opposite direction.
> >>
> >> And since the geometry to any one observer is constantly changing by
almost 180 degrees during an overhead pass, that is why it is very easy to
see, complete change in circularity.
> >>
> >> Bob, WB4APR
> >>
> >
> >
> >
> >--
> >
> >Sent from my computer.
> >
> >tom ...
> ___
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> Not an AMSAT-NA member? Join now to support the amateur satellite program!
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-05 Thread Thomas Doyle
Thanks to Domenico for sharing the work done by K4KJ. It is amazing
how much good information there is out there. It takes a bit of
digging to find it but it is worth the effort. The configuration shown
in figure 14 looks promising but probably too difficult to put on a
sat.

W9KE Tom Doyle

On Sat, Aug 4, 2012 at 10:18 PM, i8cvs  wrote:
> Hi All,
>
> I agree completely with Bob, WB4APR and this is what is wery well
> explained into the article "CIRCULAR POLARIZATION by K4KJ,
> a zipped file 5 MB long available from me.
>
> 73" de
>
> i8CVS Domenico
>
> - Original Message -
> From: "Bob Bruninga " 
> To: "Thomas Doyle" 
> Cc: ; "andrew abken" 
> Sent: Sunday, August 05, 2012 12:24 AM
> Subject: [amsat-bb] Re: Antenna Polarization Technical Question
>
>
>> > Not sure why anyone would want to maintain the
>> > orientation of the satellite in such a way that
>> > would cause the direction of circular
>> > polarization to change during the path.
>>
>> Lets try this approach... As I said before,  By the laws of physics, what
> comes out one side of a circular polarized low gain antenna as RHCP comes
> out the opposite side as LHCP.
>>
>> Now given that, and the fact that someone in Maryland is in the center of
> the RHCP beam, then by the laws of physics, the guy in California must see
> mostly LHCP.  No matter how much one of those persons demands that he
> deserves the RHCP beam, by definition, someone else somewhere will get the
> LHCP one, and the geometry changes at least every 10 minutes or so and every
> time the spacecraft rotates a bit.
>>
>> So one might say, "point it down" then only the person in Kansas will see
> the main beam and those in CA or MD will be completely off the sides almost
> 70 degrees from the main beam.  Mot people do not realize how LOW these
> satellites are.  The only solution is to put satellites so high, that "down"
> is about the same to everyone (geostationary altitude).  But then that takes
> 100 times more altitude, and that takes 10,000 times more power.
>>
>> Better to just live with the laws of physics... I guess.
>>
>> Bob, WB4aPR
>>
>> >
>> >On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
>> >>> I believe that is true but that does not explain
>> >>> why the optimum polarity setting on the receive
>> >>> end would change during a pass.
>> >>
>> >> That's easy.  The circularity on a pair of crossed dipoles (about all
> you can get on a spacecraft) May be designed for Right hand circularity when
> viewed from the prime direction.  But by definition, that save waveform will
> be LHC when viewed from the opposite direction.
>> >>
>> >> And since the geometry to any one observer is constantly changing by
> almost 180 degrees during an overhead pass, that is why it is very easy to
> see, complete change in circularity.
>> >>
>> >> Bob, WB4APR
>> >>
>> >
>> >
>> >
>> >--
>> >
>> >Sent from my computer.
>> >
>> >tom ...
>> ___
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>> Not an AMSAT-NA member? Join now to support the amateur satellite program!
>> Subscription settings: http://amsat.org/mailman/listinfo/amsat-bb
>



-- 

Sent from my computer.

tom ...
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-05 Thread Art McBride
Bob,
Just a reminder, a QFH antenna is circularly polarized over the whole
envelope of the antenna. A sharp null exists on the back side. A one
wavelength, one turn has gain at low angle side radiation and a 4 dB loss
overhead, where the distance to the ground station is the smallest.
Certainly this is a good fit for satellites.

Turnstile antennas and patch antennas are linear polarized at the sides and
of course are the easiest to implement on a satellite. 

My point is all circular antennas are not equal and having an antenna with
gain on the sides opposed to the center of the antenna is very desirable.

Art,
KC6UQH

-Original Message-
From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
Behalf Of Bob Bruninga 
Sent: Saturday, August 04, 2012 3:25 PM
To: Thomas Doyle
Cc: amsat-bb@amsat.org; andrew abken
Subject: [amsat-bb] Re: Antenna Polarization Technical Question

> Not sure why anyone would want to maintain the 
> orientation of the satellite in such a way that 
> would cause the direction of circular
> polarization to change during the path. 

Lets try this approach... As I said before,  By the laws of physics, what
comes out one side of a circular polarized low gain antenna as RHCP comes
out the opposite side as LHCP.

Now given that, and the fact that someone in Maryland is in the center of
the RHCP beam, then by the laws of physics, the guy in California must see
mostly LHCP.  No matter how much one of those persons demands that he
deserves the RHCP beam, by definition, someone else somewhere will get the
LHCP one, and the geometry changes at least every 10 minutes or so and every
time the spacecraft rotates a bit.

So one might say, "point it down" then only the person in Kansas will see
the main beam and those in CA or MD will be completely off the sides almost
70 degrees from the main beam.  Mot people do not realize how LOW these
satellites are.  The only solution is to put satellites so high, that "down"
is about the same to everyone (geostationary altitude).  But then that takes
100 times more altitude, and that takes 10,000 times more power.

Better to just live with the laws of physics... I guess.

Bob, WB4aPR

>
>On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
>>> I believe that is true but that does not explain
>>> why the optimum polarity setting on the receive
>>> end would change during a pass.
>>
>> That's easy.  The circularity on a pair of crossed dipoles (about all
you can get on a spacecraft) May be designed for Right hand circularity when
viewed from the prime direction.  But by definition, that save waveform will
be LHC when viewed from the opposite direction.
>>
>> And since the geometry to any one observer is constantly changing by
almost 180 degrees during an overhead pass, that is why it is very easy to
see, complete change in circularity.
>>
>> Bob, WB4APR
>>
>
>
>
>-- 
>
>Sent from my computer.
>
>tom ...
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[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-05 Thread i8cvs
Hi Art, KC6UQH

It is correct that a QFH is circularly polarized over the whole envelope
of the antenna.If it is left wound the polarization is RHCP and if it is
right wound the resulting polarization is LHCP.

By the way the point is the satellite antenna.

If the satellite antenna is made using two crossed dipoles mounted in the
same mechanical plane and are supplied with 90° out of phase than the
radiated polarization is RHCP along one axial direction and LHCP along
the other axial direction.

Since the satellite is thumbling orbiting in the space than the polarization
coming from the satellite to earth or coming from the ground station to
the satellite is continuing changing from RHCP to LHCP to linear passing
through elliptical.

The bad point is that a QFH can only radiate RHCP or LHCP depending
on it's winding direction so that using only one QFH the QSB generated
by the satellite thumbling cannot be completely eliminated and two
switchable QFH's one RHCP and the other one LHCP would be necessary.

73" de

i8CVS Domenico

- Original Message -
From: "Art McBride" 
To: "'Bob Bruninga '" ; "'Thomas Doyle'"

Cc: ; "'andrew abken'" 
Sent: Sunday, August 05, 2012 10:44 PM
Subject: [amsat-bb] Re: Antenna Polarization Technical Question


> Bob,
> Just a reminder, a QFH antenna is circularly polarized over the whole
> envelope of the antenna. A sharp null exists on the back side. A one
> wavelength, one turn has gain at low angle side radiation and a 4 dB loss
> overhead, where the distance to the ground station is the smallest.
> Certainly this is a good fit for satellites.
>
> Turnstile antennas and patch antennas are linear polarized at the sides
and
> of course are the easiest to implement on a satellite.
>
> My point is all circular antennas are not equal and having an antenna with
> gain on the sides opposed to the center of the antenna is very desirable.
>
> Art,
> KC6UQH
>
> -Original Message-
> From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
> Behalf Of Bob Bruninga
> Sent: Saturday, August 04, 2012 3:25 PM
> To: Thomas Doyle
> Cc: amsat-bb@amsat.org; andrew abken
> Subject: [amsat-bb] Re: Antenna Polarization Technical Question
>
> > Not sure why anyone would want to maintain the
> > orientation of the satellite in such a way that
> > would cause the direction of circular
> > polarization to change during the path.
>
> Lets try this approach... As I said before,  By the laws of physics, what
> comes out one side of a circular polarized low gain antenna as RHCP comes
> out the opposite side as LHCP.
>
> Now given that, and the fact that someone in Maryland is in the center of
> the RHCP beam, then by the laws of physics, the guy in California must see
> mostly LHCP.  No matter how much one of those persons demands that he
> deserves the RHCP beam, by definition, someone else somewhere will get the
> LHCP one, and the geometry changes at least every 10 minutes or so and
every
> time the spacecraft rotates a bit.
>
> So one might say, "point it down" then only the person in Kansas will see
> the main beam and those in CA or MD will be completely off the sides
almost
> 70 degrees from the main beam.  Mot people do not realize how LOW these
> satellites are.  The only solution is to put satellites so high, that
"down"
> is about the same to everyone (geostationary altitude).  But then that
takes
> 100 times more altitude, and that takes 10,000 times more power.
>
> Better to just live with the laws of physics... I guess.
>
> Bob, WB4aPR
>
> >
> >On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga  wrote:
> >>> I believe that is true but that does not explain
> >>> why the optimum polarity setting on the receive
> >>> end would change during a pass.
> >>
> >> That's easy.  The circularity on a pair of crossed dipoles (about all
> you can get on a spacecraft) May be designed for Right hand circularity
when
> viewed from the prime direction.  But by definition, that save waveform
will
> be LHC when viewed from the opposite direction.
> >>
> >> And since the geometry to any one observer is constantly changing by
> almost 180 degrees during an overhead pass, that is why it is very easy to
> see, complete change in circularity.
> >>
> >> Bob, WB4APR
> >>
> >
> >
> >
> >--
> >
> >Sent from my computer.
> >
> >tom ...
> ___
> Sent via AMSAT-BB@amsat.org. Opinions expressed are those of the author.
> Not an AMSAT-NA member? Join now to support the amateur satellite program!
> Subsc

[amsat-bb] Re: Antenna Polarization Technical Question

2012-08-05 Thread Art McBride
Domenico,

You are correct, the crossed dipoles fed in quadrature when on axis exhibit
LH and RH circular patterns, but 90 degrees from axis they are linearly
polarized. This gives poor performance at low angles as well as requiring
both RH and LH rotations for a full pass reception. 

Obviously the QFH antenna to be effective should point down at the earth,
with the sides pointing to the horizon and the backside towards outer space.
The one wave one turn can be optimized,(Length to Diameter ratio)to provide
best radiation at the horizon. This will give good performance when the
satellite is near zenith as well as provide improved performance at low
elevations.

Circular polarization does help to eliminate multipath and provide a steady
copy, even while the antenna is mechanically rotating with the satellite for
stabilization and temperature stability. 

Art,
KC6UQH

-Original Message-
From: i8cvs [mailto:domenico.i8...@tin.it] 
Sent: Sunday, August 05, 2012 3:27 PM
To: AMSAT-BB; Bob Bruninga ; kc6...@cox.net; Thomas Doyle
Subject: Re: [amsat-bb] Re: Antenna Polarization Technical Question

Hi Art, KC6UQH

It is correct that a QFH is circularly polarized over the whole envelope
of the antenna.If it is left wound the polarization is RHCP and if it is
right wound the resulting polarization is LHCP.

By the way the point is the satellite antenna.

If the satellite antenna is made using two crossed dipoles mounted in the
same mechanical plane and are supplied with 90° out of phase than the
radiated polarization is RHCP along one axial direction and LHCP along
the other axial direction.

Since the satellite is thumbling orbiting in the space than the polarization
coming from the satellite to earth or coming from the ground station to
the satellite is continuing changing from RHCP to LHCP to linear passing
through elliptical.

The bad point is that a QFH can only radiate RHCP or LHCP depending
on it's winding direction so that using only one QFH the QSB generated
by the satellite thumbling cannot be completely eliminated and two
switchable QFH's one RHCP and the other one LHCP would be necessary.

73" de

i8CVS Domenico

- Original Message -
From: "Art McBride" 
To: "'Bob Bruninga '" ; "'Thomas Doyle'"

Cc: ; "'andrew abken'" 
Sent: Sunday, August 05, 2012 10:44 PM
Subject: [amsat-bb] Re: Antenna Polarization Technical Question


> Bob,
> Just a reminder, a QFH antenna is circularly polarized over the whole
> envelope of the antenna. A sharp null exists on the back side. A one
> wavelength, one turn has gain at low angle side radiation and a 4 dB loss
> overhead, where the distance to the ground station is the smallest.
> Certainly this is a good fit for satellites.
>
> Turnstile antennas and patch antennas are linear polarized at the sides
and
> of course are the easiest to implement on a satellite.
>
> My point is all circular antennas are not equal and having an antenna with
> gain on the sides opposed to the center of the antenna is very desirable.
>
> Art,
> KC6UQH
>
> -Original Message-
> From: amsat-bb-boun...@amsat.org [mailto:amsat-bb-boun...@amsat.org] On
> Behalf Of Bob Bruninga
> Sent: Saturday, August 04, 2012 3:25 PM
> To: Thomas Doyle
> Cc: amsat-bb@amsat.org; andrew abken
> Subject: [amsat-bb] Re: Antenna Polarization Technical Question
>
> > Not sure why anyone would want to maintain the
> > orientation of the satellite in such a way that
> > would cause the direction of circular
> > polarization to change during the path.
>
> Lets try this approach... As I said before,  By the laws of physics, what
> comes out one side of a circular polarized low gain antenna as RHCP comes
> out the opposite side as LHCP.
>
> Now given that, and the fact that someone in Maryland is in the center of
> the RHCP beam, then by the laws of physics, the guy in California must see
> mostly LHCP.  No matter how much one of those persons demands that he
> deserves the RHCP beam, by definition, someone else somewhere will get the
> LHCP one, and the geometry changes at least every 10 minutes or so and
every
> time the spacecraft rotates a bit.
>
> So one might say, "point it down" then only the person in Kansas will see
> the main beam and those in CA or MD will be completely off the sides
almost
> 70 degrees from the main beam.  Mot people do not realize how LOW these
> satellites are.  The only solution is to put satellites so high, that
"down"
> is about the same to everyone (geostationary altitude).  But then that
takes
> 100 times more altitude, and that takes 10,000 times more power.
>
> Better to just live with the laws of physics... I guess.
>
> Bob, WB4aPR
>
> >
> >On Sat, Aug 4, 2012 at 2:47 PM, Bob Bruninga