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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