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	<title>Comments for The Nog</title>
	<atom:link href="http://blogs.agi.com/navigationAccuracy/?feed=comments-rss2" rel="self" type="application/rss+xml" />
	<link>http://blogs.agi.com/navigationAccuracy</link>
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		<title>Comment on GPS Basics by Ted Driver</title>
		<link>http://blogs.agi.com/navigationAccuracy/?page_id=6&#038;cpage=1#comment-24598</link>
		<dc:creator>Ted Driver</dc:creator>
		<pubDate>Fri, 29 Apr 2011 16:00:43 +0000</pubDate>
		<guid isPermaLink="false">http://bloghost.stk.com/navigationAccuracy/?page_id=6#comment-24598</guid>
		<description>lily,
A Least-squares formulation used used, such as can be found in books like: 
&lt;ul&gt;
Global Positioning System, Signals, Performance and Analysis&lt;/ul&gt;
by Misra, Enge</description>
		<content:encoded><![CDATA[<p>lily,<br />
A Least-squares formulation used used, such as can be found in books like: </p>
<ul>
Global Positioning System, Signals, Performance and Analysis</ul>
<p>by Misra, Enge</p>
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		<title>Comment on GPS Basics by lily</title>
		<link>http://blogs.agi.com/navigationAccuracy/?page_id=6&#038;cpage=1#comment-24042</link>
		<dc:creator>lily</dc:creator>
		<pubDate>Sat, 26 Mar 2011 04:32:50 +0000</pubDate>
		<guid isPermaLink="false">http://bloghost.stk.com/navigationAccuracy/?page_id=6#comment-24042</guid>
		<description>thank for your information above. i want to ask, what formula you use to calculate position error once we know GDOP?
tks</description>
		<content:encoded><![CDATA[<p>thank for your information above. i want to ask, what formula you use to calculate position error once we know GDOP?<br />
tks</p>
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		<title>Comment on GPS constellation optimization analysis by MPacheco</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=315&#038;cpage=1#comment-20218</link>
		<dc:creator>MPacheco</dc:creator>
		<pubDate>Wed, 04 Aug 2010 04:15:35 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=315#comment-20218</guid>
		<description>Subject: SVN62 placement

Looking at FAA&#039;s WAAS Satellite Status page, it looks like the new IIF SV1 satellite is right on top of PRN 30 (SVN 30).
http://www.nstb.tc.faa.gov/incoming/waas_sats.png

Considering:
1 - There&#039;s already PRN12 close by
2 - The constellation optimization effort

Then why not position PRN 25 halfway between PRN 12 and PRN 16, so that it make the best possible contribution to the constellation ??? I&#039;m assuming that PRN30 is the next satellite to be retired before IIF SV2 is launched, considering that we&#039;re at the 32 PRN limit. Even if there are concerns about PRN12&#039;s longevity, wouldn&#039;t PRN30 be kept in residual status ?

I was under the impression that newer satellites would be positioned in a spread out configuration, providing for much better overall GPS geometry.

Perhaps this was just a launch issue, and IIF SV1 is about to the repositioned on a smarted position for optimum contribution to the GPS constellation.</description>
		<content:encoded><![CDATA[<p>Subject: SVN62 placement</p>
<p>Looking at FAA&#8217;s WAAS Satellite Status page, it looks like the new IIF SV1 satellite is right on top of PRN 30 (SVN 30).<br />
<a href="http://www.nstb.tc.faa.gov/incoming/waas_sats.png" rel="nofollow">http://www.nstb.tc.faa.gov/incoming/waas_sats.png</a></p>
<p>Considering:<br />
1 &#8211; There&#8217;s already PRN12 close by<br />
2 &#8211; The constellation optimization effort</p>
<p>Then why not position PRN 25 halfway between PRN 12 and PRN 16, so that it make the best possible contribution to the constellation ??? I&#8217;m assuming that PRN30 is the next satellite to be retired before IIF SV2 is launched, considering that we&#8217;re at the 32 PRN limit. Even if there are concerns about PRN12&#8242;s longevity, wouldn&#8217;t PRN30 be kept in residual status ?</p>
<p>I was under the impression that newer satellites would be positioned in a spread out configuration, providing for much better overall GPS geometry.</p>
<p>Perhaps this was just a launch issue, and IIF SV1 is about to the repositioned on a smarted position for optimum contribution to the GPS constellation.</p>
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		<title>Comment on GPS Error Budget by Parimal</title>
		<link>http://blogs.agi.com/navigationAccuracy/?page_id=35&#038;cpage=1#comment-19890</link>
		<dc:creator>Parimal</dc:creator>
		<pubDate>Mon, 19 Jul 2010 11:29:09 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?page_id=35#comment-19890</guid>
		<description>pl share information about GNSS I am designer of IRNSS payload form ISRO

parimal majithiya</description>
		<content:encoded><![CDATA[<p>pl share information about GNSS I am designer of IRNSS payload form ISRO</p>
<p>parimal majithiya</p>
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		<title>Comment on SVN 49, PRN 1 URE too high by MPacheco</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=184&#038;cpage=1#comment-19055</link>
		<dc:creator>MPacheco</dc:creator>
		<pubDate>Thu, 17 Jun 2010 22:39:40 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=184#comment-19055</guid>
		<description>In that case, AFAIK, SVN49 isn&#039;t going to be very useful at all for the GPS community. WAAS and EGNOS won&#039;t use it (Raytheon/FAA/ESA already stated that). In the end it might be useful only for the standard, non precision user, and to a user faced with no fix without SVN49, using it as a last resort.

It seems to me that most IIR/IIRM (all except for SVN42/49) are still in perfect shape (I&#039;m assuming since there&#039;s no information to the contrary), when the 12 IIF are all in orbit, then all IIA&#039;s will be decommissioned/put in residual status (there&#039;s 11 IIFs to be launched and 11 IIAs left in operational status). Perhaps the first IIIA might be launched to take SVN49&#039;s place and put SVN49 in residual status as well... It&#039;s interesting that the latest IIF launch in slot B2 is just ahead of SVN49&#039;s B6. Once IIF-1 is operational, couldn&#039;t PRN30 (currently operational in slot B2) be moved from B2 to B6 ?</description>
		<content:encoded><![CDATA[<p>In that case, AFAIK, SVN49 isn&#8217;t going to be very useful at all for the GPS community. WAAS and EGNOS won&#8217;t use it (Raytheon/FAA/ESA already stated that). In the end it might be useful only for the standard, non precision user, and to a user faced with no fix without SVN49, using it as a last resort.</p>
<p>It seems to me that most IIR/IIRM (all except for SVN42/49) are still in perfect shape (I&#8217;m assuming since there&#8217;s no information to the contrary), when the 12 IIF are all in orbit, then all IIA&#8217;s will be decommissioned/put in residual status (there&#8217;s 11 IIFs to be launched and 11 IIAs left in operational status). Perhaps the first IIIA might be launched to take SVN49&#8242;s place and put SVN49 in residual status as well&#8230; It&#8217;s interesting that the latest IIF launch in slot B2 is just ahead of SVN49&#8242;s B6. Once IIF-1 is operational, couldn&#8217;t PRN30 (currently operational in slot B2) be moved from B2 to B6 ?</p>
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		<title>Comment on What&#8217;s the difference between SEM and YUMA almanacs? by Tony Babiarz</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=113&#038;cpage=1#comment-18719</link>
		<dc:creator>Tony Babiarz</dc:creator>
		<pubDate>Wed, 09 Jun 2010 15:44:35 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=113#comment-18719</guid>
		<description>Define SEM - the word.  S________ E________ M_______?

Define YUMA - the word  Y________ U________ M_______ A________?</description>
		<content:encoded><![CDATA[<p>Define SEM &#8211; the word.  S________ E________ M_______?</p>
<p>Define YUMA &#8211; the word  Y________ U________ M_______ A________?</p>
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		<title>Comment on What&#8217;s the difference between SEM and YUMA almanacs? by Propagator</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=113&#038;cpage=1#comment-18381</link>
		<dc:creator>Propagator</dc:creator>
		<pubDate>Wed, 12 May 2010 19:36:12 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=113#comment-18381</guid>
		<description>Very useful, thank you!</description>
		<content:encoded><![CDATA[<p>Very useful, thank you!</p>
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		<title>Comment on SVN 49, PRN 1 URE too high by Ted Driver</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=184&#038;cpage=1#comment-16023</link>
		<dc:creator>Ted Driver</dc:creator>
		<pubDate>Sun, 28 Mar 2010 13:43:19 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=184#comment-16023</guid>
		<description>Good idea!  But, there is no chance that could happen - for at least three reasons.  First and foremost, the Shuttle is not designed to travel to the heights the GPS satellite&#039;s orbits reside in.  The farthest the shuttle ever went was to service the Hubble Space Telescope, which still isn&#039;t near the GPS satellites.  Next, the last Shuttle mission will occur this year.  With no more funding for the shuttle, it won&#039;t be going anywhere.  Third, even if it were possible to get there, the severity of the L5 problem on SVN 49 doesn&#039;t warrant the cost of removing the L5 demo payload.  Servicing a satellite in orbit is very tricky and damage can occur easily.</description>
		<content:encoded><![CDATA[<p>Good idea!  But, there is no chance that could happen &#8211; for at least three reasons.  First and foremost, the Shuttle is not designed to travel to the heights the GPS satellite&#8217;s orbits reside in.  The farthest the shuttle ever went was to service the Hubble Space Telescope, which still isn&#8217;t near the GPS satellites.  Next, the last Shuttle mission will occur this year.  With no more funding for the shuttle, it won&#8217;t be going anywhere.  Third, even if it were possible to get there, the severity of the L5 problem on SVN 49 doesn&#8217;t warrant the cost of removing the L5 demo payload.  Servicing a satellite in orbit is very tricky and damage can occur easily.</p>
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		<title>Comment on SVN 49, PRN 1 URE too high by MPacheco</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=184&#038;cpage=1#comment-15955</link>
		<dc:creator>MPacheco</dc:creator>
		<pubDate>Sat, 27 Mar 2010 23:35:58 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=184#comment-15955</guid>
		<description>Is there any chance at all, that with a successful launch of IIF-1, with a properly tested L5 payload, that a subsequent Space Shuttle mission could remove the L5 demo payload (space walk) restoring SVN49 into a standard, high quality GPS satellite ? No one have questioned that so far, so what the hell...</description>
		<content:encoded><![CDATA[<p>Is there any chance at all, that with a successful launch of IIF-1, with a properly tested L5 payload, that a subsequent Space Shuttle mission could remove the L5 demo payload (space walk) restoring SVN49 into a standard, high quality GPS satellite ? No one have questioned that so far, so what the hell&#8230;</p>
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		<title>Comment on SEM and YUMA almanacs&#8230;they USED to give similar results&#8230;. by Vladislav35</title>
		<link>http://blogs.agi.com/navigationAccuracy/?p=65&#038;cpage=1#comment-15500</link>
		<dc:creator>Vladislav35</dc:creator>
		<pubDate>Tue, 16 Mar 2010 20:35:23 +0000</pubDate>
		<guid isPermaLink="false">http://blogs.agi.com/navigationAccuracy/?p=65#comment-15500</guid>
		<description>&lt;a href=&quot;http://all4webmaster.ru/&quot; rel=&quot;nofollow&quot;&gt;Я писал что-то подобное, но у Вас тема более глубого раскрыта&lt;/a&gt;</description>
		<content:encoded><![CDATA[<p><a href="http://all4webmaster.ru/" rel="nofollow">Я писал что-то подобное, но у Вас тема более глубого раскрыта</a></p>
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