[Cesg-all] Re: Rick Schnurr's comments re: AOS Pink Sheets
Greg J Kazz
greg.j.kazz@jpl.nasa.gov
Tue, 15 Jul 2003 12:58:44 -0700
At 7/15/2003 11:53 AM, Adrian J. Hooke wrote:
>At 10:12 AM 7/15/2003, Greg J Kazz wrote:
>>** The rationale for this field is to allow high rate mission to have a
>>sequence counter that doesn't rollover during a pass.
>
>Any counter will roll over eventually - it depends on the frame length and
>the data rate. If I punched the buttons on my trusty Casio wrist
>communicator properly, a 2**27 counter rolls over in 3.8 hours if the
>frame length is 10K bits and the data rate is 100Mb/s. That's a data rate
>that we may see from Mars in the lifetime of this standard.
>
>Surely there are other ways to handle rollover. For instance, why not
>switch to another Virtual Channel when rollover occurs? You've got 64 of
>those buggers to use, and presumably right now most of them are going unused.
>
>And anyway, what's the problem if the counter *does* roll over? Don't we
>have other ground mechanisms to detect this?
** It's a flight system issue. The flight system requires a simple method
for identifying AOS frames for retransmission. **
>>Those missions that do not require the extra field, simply set it to all
>>zeros, which they currently do today, because it is defined as a spare.
>>Those that do use it, will increment those bits accordingly. **
>
>But how does the receiver know whether this field is used or not?
>Whichever way you look at it, you're running a different protocol with a
>24-bit counter than you are with a 27-bit counter. Different protocols are
>normally signalled to the receiver. How is the signalling done in your
>proposal?
** Ground operations could be managed if required for retransmission
support. **
>>** AOS was designed for SSF and ESA 's Hercules. Not a large contingent
>>of users. **
>
>I don't understand this. Since it has an 8-bit SCID, the AOS frame can
>handle another 254 spacecraft before we run out of unique spacecraft
>names. AOS can certainly accommodate an order of magnitude more user
>spacecraft than anyone currently has on the drawing board. ** yes the
>capability is there, just pointing out that the user community for AOS
>today is rather small **
>
>>This would also benefit missions flying SSRs using AOS frame retransmission.
>
>No doubt. But then why don't you package this change as part of an omnibus
>proposal that adds the AOS retransmission procedures *and* the capability
>to handle higher data rates? And in the process, why don't you update the
>whole AOS recommendation (http://www.ccsds.org/documents/701x0b3.pdf) to
>reflect this omnibus change, including a complete re-write of para.
>5.4.9.2.2 and the entire Section 6 -- which already contains an incomplete
>definition of a Space Link ARQ Procedure? Otherwise it will surely be
>extremely confusing to a user to see two separate ARQ mechanisms in the
>specification, and no way to differentiate between them. ** Actually this
>book is dead and has been woefully out of date for a long time. Part of
>the problem is retiring the old AOS book and making changes to Yamada's
>restructured book from this point on. SLS-WG is working with Tom G. on how
>best to procede on this. **
> **
>
>Greg, I don't want to be a pill about this, but there is a lot at stake
>here in terms of controlling the quality of our products. If I am missing
>something, please correct me.
>
>///adrian