Can Astronauts Use GPS To Navigate On the Moon? (ieee.org) 99
schwit1 shares a report from IEEE Spectrum: Here on Earth, our lives have been transformed by the Global Positioning System, fleets of satellites operated by the United States and other countries that are used in myriad ways to help people navigate. Down here, GPS is capable of pinpointing locations with accuracy measured in centimeters. Could it help astronauts on lunar voyages? Kar-Ming Cheung and Charles Lee of NASA's Jet Propulsion Laboratory in California did the math, and concluded that the answer is yes: Signals from existing global navigation satellites near the Earth could be used to guide astronauts in lunar orbit, 385,000 km away. The researchers presented their newest findings at the IEEE Aerospace Conference in Montana this month.
Cheung and Lee plotted the orbits of navigation satellites from the United States's Global Positioning System and two of its counterparts, Europe's Galileo and Russia's GLONASS system -- 81 satellites in all. Most of them have directional antennas transmitting toward Earth's surface, but their signals also radiate into space. Those signals, say the researchers, are strong enough to be read by spacecraft with fairly compact receivers near the moon. Cheung, Lee and their team calculated that a spacecraft in lunar orbit would be able to "see" between five and 13 satellites' signals at any given time -- enough to accurately determine its position in space to within 200 to 300 meters. In computer simulations, they were able to implement various methods for improving the accuracy substantially from there.
Cheung and Lee plotted the orbits of navigation satellites from the United States's Global Positioning System and two of its counterparts, Europe's Galileo and Russia's GLONASS system -- 81 satellites in all. Most of them have directional antennas transmitting toward Earth's surface, but their signals also radiate into space. Those signals, say the researchers, are strong enough to be read by spacecraft with fairly compact receivers near the moon. Cheung, Lee and their team calculated that a spacecraft in lunar orbit would be able to "see" between five and 13 satellites' signals at any given time -- enough to accurately determine its position in space to within 200 to 300 meters. In computer simulations, they were able to implement various methods for improving the accuracy substantially from there.
Lol, sure, if... (Score:2, Interesting)
Sometimes even NASA forgets to take those relative speed differences into account and have to deal with it after the fact.
(Once they realize what was wrong in the first place.)
Don't forget, the GPS sate
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Re:Lol, sure, if... (Score:5, Interesting)
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Re:Lol, sure, if... (Score:5, Insightful)
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I did, but then I immediately tested positive to a drug test.
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... matter of fact it's all dark.
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Of course there's a dark side of the moon. Did you think that somehow sunlight magically curves around nothing to shine on all sides of the orb simultaneously, but only for the moon?
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There most certainly is a light and dark side of the moon. Much of the area on the near side of the moon is basaltic maria and has a lower albedo than the far side.
The side we see from Earth is in fact the dark side of the moon.
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Re: Lol, sure, if... (Score:2)
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God, wake up sheeple. The Moon is flat.
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And made from cheese, I'm just not sure about the brand!
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Maybe we should call it the “far side of the moon” instead? Relative to the Earth of course.
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There is no "darkside" of the moon.
Sure there is.
During a full moon, it's the far side.
During a new moon, it's the side facing the earth.
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If you can pick up the signal of at least 3 of the GPS satellites, and you're GPS device is set to compensate for being outside their orbits, and for the relativistic shifts due to speed and direction differences due to the moon, or your orbit of the moon if you haven't landed yet, then sure, it'll work fine.
Sometimes even NASA forgets to take those relative speed differences into account and have to deal with it after the fact.
(Once they realize what was wrong in the first place.)
Don't forget, the GPS satellites are geosynchronous with Earth, NOT Luna.
I thought there were some speed and height limitations on GPS where it wouldn't work anymore.
Maybe it's just the civilian side.
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I thought there were some speed and height limitations on GPS where it wouldn't work anymore.
Maybe it's just the civilian side.
I think that's on the receivers, to make sure the answer they give is plausible. With 4 satellites there are actually two solutions in space and time, but one of them will be outside the satellites' orbit and would vary wildly if it's the wrong solution (which it will be for terrestrial users). The satellites don't care (or know) where you are or how fast you're travelling.
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Yes, you're correct. But also, most civilian receivers are/were nerfed to stop naughty people using them in missile guidance systems.
No problem for well-financed "terrorists" backed by a large nation-state, of course.
(If you can build a device capable of > 1000 Knots and >18Km then figuring out the GPS is probably the least of your worries...)
"In GPS technology, the phrasing “COCOM Limits” is also used to refer to a limit placed to GPS tracking devices that should disable tracking when th
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But also, most civilian receivers are/were nerfed to stop naughty people using them in missile guidance systems.
No, civilian GPS are not "nerfed".
In earlier times, they simply sent a wrong signal, which made you displaced by a few hundert meters. Military GPS knew the displacement and could calculate the correct coordinates. The displacement was planet wide a fixed offset, so local governments came to the idea to set up a reference point. E.g. you take a mountain which is high enough to cover about 100km (o
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That is nonsense. An ICBM enters the atmosphere under so much speed that it is surrounded by ionized gases, receiving GPS signals is impossible in such circumstances. And the ability to hit a target always was already in the 10m range long before GPS even existed.
The realities of the physics did not in any way interfere with Congress's ability to pass a law. Which they did. The law exists. Civilian GPS receivers comply with it. Is it a useless and silly restriction? Yes. When has that ever stopped Congress?
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There are other restriction as well like civilian receivers may not use a antenna phasing for jam resistance which is too bad since it would help considerably with multipath distortion in cities.
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The reason is not technical, but is instead a legal mandate that receivers should not work above certain altitudes and speeds to prevent their use in weapons systems. These COCOM limits are frequently a problem for amateur rocketry and high altitude balloon launches and other civilian aerospace users. Although it's "law," receivers often implement their enforcement (if any) in nonstandard ways. It is easy to find receivers that are not limited, and there are open source GNSS hardware and software receivers
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So, only applies to equipment manufactured by US-interacting corporations.
Waiting for Huawei to release an unrestricted GPS receiver/ decoder ASIC for use world-wide, with a drop-in replacement for more popular restricted ASICs. They have a significant amount to gain, and nothing to lose. Sell them at a lower price than a Motorola (or other re
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The "civilian side" (AKA Selective Availability) has been turned off for almost 20 years.
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Ahh, yes. I remember as well when this was disabled: it was too troublesome to enable that higher availability mode for military equipment, supplying and maintaining the decryption keys, so it was left enabled for everyont.
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They're not talking about SA, they're talking about COCOM restrictions on GPS receivers. GPS receivers are supposed to refuse to operate at high altitudes and speeds as part of arms export regulations.
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There are (or used to be) limits in the domestic GPS receivers to stop other nations using them for ballistic missile guidance, just search for COCOM limits on GPS.
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I thought there were some speed and height limitations on GPS where it wouldn't work anymore.
No.
The problem in this case is that only satellites that are "behind" the earth but not covered by the earth can be "seen" from the moon as they direct their signals to earth and by missing earth and hitting the moon you can calculate your position. But I doubt it will have cm accuracy.
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Receiving the signals around the limb of the Earth would likely exacerbate the ranging distortions that the ionosphere imposes on the position solutions---worse than an Earthbound receiver would see as the signals traverse even more ionosphere. I understanding that the positioning accuracy that the paper presented was/is around 300m---which is about what the original design spec assumed would be available using the C/A code tracking. SA came about when the original user equipment was found to be performing
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If you can pick up the signal of at least 3 of the GPS satellites, and you're GPS device is set to compensate for being outside their orbits, and for the relativistic shifts due to speed and direction differences due to the moon, or your orbit of the moon if you haven't landed yet, then sure, it'll work fine.
About half the constellation should be visible from the moon at any time, so seeing 4 (3 is not enough) satellites should be no issue. And I doubt NASA would be planning on buying an off-the-shelf receiver from Amazon. The biggest issue I can see is that the dilution of precision would be poor because the satellites would all be in pretty much the same direction.
Re: Lol, sure, if... (Score:1)
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Actually, the only satellites that are useable are the ones on the far side of the Earth. The half youre talking about have their backs toward the moon. GPS satellites beam their signals with highly directional antennas down toward the surface. Spacecraft have to use the sats on the far side of the planet which are pointing their antennas their way but are visible over the limb of the planet.
Surely they're not so directional that the earth's attenuation is less significant than the sidelobes? The transmitters would need a massive aperture for that to be the case.
*NOT* GeoSync (Score:5, Informative)
Don't forget, the GPS satellites are geosynchronous with Earth, NOT Luna.
None of the satelite positioning system (GPS, Glonass, Galileo, Beidu, etc.) is on a geosynchronous orbit.
That's why you need to have an ephemeris table (either fetched from the internet or downstreamed at snail pace from the sats themselves).
That's why the actual visible sattelite at any fixed position change over time.
That's also why they work at any position on the earth surface, including the poles (Well for the networks that have enough coverage, at least).
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Half-sphere signal (Score:2)
The question I have, though, is whether the GPS satellites' antennae emit in the proper direction to be detectable from the Moon. If they're designed to focus their transmission down,
That's already addressed even in the summary:
I wouldn't be expecting positioning satellite to be extremely focused, because (unlike, say some type of communication) a positioning receiver ideally isn't only listening to the satellite most straight above (though it migh
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On the gripping hand, putting a couple of GPS-series satellites into Earth-Moon L4,5 positions, pointing at the Moon, would considerably improve all aspects of the location.
Actually, putting one at L4 (or L5) and one at L2 would probably help even more, but the L2 one wouldn'
Fixed sattelite not needed. (Score:2)
On the gripping hand, putting a couple of GPS-series satellites into Earth-Moon L4,5 positions, pointing at the Moon, would considerably improve all aspects of the location.
Again, positioning system satellites aren't geostationary, you DO NOT need to have them at fixed position in the sky. Thus you do not need them at Lagrange point. You could just have a couple of extra satellite orbiting the Moon and increasing the precision.
Actually, putting one at L4 (or L5) and one at L2 would probably help even more, but the L2 one wouldn't have an obvious directional preference, so you'd need a pretty wide-angle antenna on the feed, with consequences for range.
The only interest of putting precision-enhancing positioning satellite at lagrange points in the future is if there are some future misson going there [wikipedia.org] and you could piggy back a GPS emitter on them.
Now the thing is, if you're considering piggy backing,
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I know that. You're confusing me with someone who misunderstands that point. I've dispensed corrective messages to others in this thread on that point.
A satellite at one of the Lagrange points would need station-keeping fuel and an ephemeris equation in the receivers in any case ; it's position on the sky would always be varying, just not as much as the position of a terrestrial GPS satel
Re: Lol, sure, if... (Score:2)
Me reading headline: "What?!? Of course not!"
Me reading article: "Whoa dude that's some impressive work..."
They took all the things you mention into account and still think it's possible.
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They took all the things you mention into account and still think it's possible.
Unpossible. The world's subject matter experts in every field are exclusive to Slashdot comment boxes.
Re: Lol, sure, if... (Score:1)
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Specifically, which spacecraft, whose orbital position is not already known to sufficient precision from the ephemeris calculated from their actual launch parameters (not the calculated parameters, because not all cores of a booster stage fire).
Spacecraft do have their ephemerides updated, regularly, but TTBOMK that it the result of either horizon-crossing of the radio detectability ( a very cheap on/ off + clock measurement) or optical/ radio positioning in the sky (needs "setting circl
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It's possible (for someone who knows a lot more than me) to build your own GPS receiver from first principals, which avoids the limits placed on commercial receivers (>1900km/s and/or >18,000m). Here's an example [aholme.co.uk] which uses a custom FPGA board, coupled to a Raspberry Pi. If a sufficiently dedicated and knowledgable person can build one at home, I suspect a satelli
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Agreed, as long as you are including the ionosphere in your atmosphere. Which most people do accidentally, but in this case, it is significant - a large (the largest?) part of the jitter in a received GPS signal is in delay of nanoseconds in transmission through the 70km+(?) ionosphere, giving much of the ~10m raw uncertainty in a GPS location. But if you nail a GPS rece
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Uh. No they're not. Their semi-synchronous (12 hour orbits). Gawd. I hope NASA didn't forget to take that into account.
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For a semi-geosynchronous satellite, in the same position twice daily, if your receiver's beam width is (say) 10 degrees (about your fist-width at arm's length), then your receiver/ transmitter will connect for [maths: day_length * 2(twice-daily) * (10/360) * (beam size)]
or [maths : day_length * 0.50505...]
Is 5% of a day nearly equivalent to 100% of a day? If you still think
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Geosynchronous means not only that the satellite orbits the earth, but also that its period of rotation about the Earth is such that its position over the surface of the earth does not change. The other word that is often used is geostationary. A geosynchronous/geos
Geosynchronous v geostationary (Score:2)
Geostationary is not the same as geosynchronous.
Geostationary means that the period is 24 hours and the orbital inclination is 0 degrees (aligned with the equator). These orbits keep the satellite constantly over the same point above the equator. This is where you find most communication satellites.
Geosynchronous means only that the orbital period is 24 hours. Since these orbits can be inclined, they do not always keep their satellites over the same spot on the surface of the Earth.
Geostationary orbits a
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That does rather propose an amusing experiment.
Hmmm. Do you remember the geometric concept of "duals" [polygons, polyhedra, curves, surfaces where (measure-point to centre) * (measure-point to dual-point) = constant (IIRC) ? So, I think that f
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Alternatively, do forget that, because it's completely untrue.
In fact, Even if some GPS satellites were geosynchronous, you'd still need at least two on the sky visible from your location which are off the celestial equator.
Unless my memory is wildly wrong, all satillites of all the GPS constellations are on orbits inclined about 60 degrees to the celestial equator (the exact number varies for constellation).
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That'd Be Fun (Score:2)
What about the Solar System? (Score:2)
It's only a matter of time before we have the technology to power our way from planet to plant without necessarily relying on orbital mechanics and gravity boosts. Mars will be at X spot in two months, point the ship and go.
This might require many navigational beacons placed strategically throughout the solar system
I wonder if any enterprising scientist at Jet Propulsion Labs or NASA have given this any kind of theoretical thought.
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> It's only a matter of time before we have the technology to power our way from planet to plant without necessarily relying on orbital mechanics and gravity boosts.
The alchemists of the ancient world also doubtless believed that transmuting lead to gold was only a matter of time. We've learned enough to understand the mechanics, but the energy costs remain outrageous and uneconomical.
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And the world is flat, Sea monsters be there, etc.
Plasma Drives [wikipedia.org], Ion Drives [wikipedia.org], etc. When you can lift a gigawatt reactor into space and make it the heart of the ship, then you suddenly have lots of energy.
BTW, you can turn lead into gold now [thoughtco.com].
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We actually have the technology, since decades.
E.g. a rocket engine based on nuclear decay, fueled with water ... Someone already answered to you with the plasma engine ... and yes the vasimir engine is more than a decade old. A nuclear decay based engine is probably the most primitive engine thinkable ... only "NIMBY" reasons and the question how to refuel it (it likely has not enough power to launch with water from earth) are preventing us building one.
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We already have myriad navigational points throughout the solar system, they're called planets and we know very precisely where they are at any particular moment. No beacon is necessary as long as the sun is still shining on them.
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The necessary code was published away back in the early 1990s. It is public domain - government un-classified work.
"Point the ship, light blue touch-paper and go" is possible. If you want to waste money. The reason that complex route are chosen are for either faster delivery (for a given payload and launch vehicle) or cheaper deliver (given payload and flexible arrival time.
it is not a pro
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This is way cool (Score:2)
Google Maps (Score:1)
Choose starting point: this crater
Choose destination: that crater over there
No but GPS can be used to navigate Uranis... (Score:1)
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Oh, that joke stinks.
GPS with local navigation beacons? (Score:2)
100 to 200 meters is fine for determining orbital positions, but isn't great if you're trying to land in a particular location.
Maybe there's a case for sending out automated landers with GPS receivers around any planned landing site. They can acquire enough GPS location fixes over a few months to measure their exact location then provide simple RF beacons for accurate local navigation within less than a meter.
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100 to 200 meters is fine for determining orbital positions, but isn't great if you're trying to land in a particular location.
Maybe there's a case for sending out automated landers with GPS receivers around any planned landing site. They can acquire enough GPS location fixes over a few months to measure their exact location then provide simple RF beacons for accurate local navigation within less than a meter.
Or, they could just output some signals that can be used for landing guides. There's no need for the beacons to know where they are relative to earth.
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Yes, I used to do GPS differential correction on data all the time back when I was surveying. We used to have to do it manually after collection with the old Trimble units. Now, they can use ground stations in real time, although it's not as accurate as doing it after the fact.
Real time DGPS from a couple moon ground stations could probably cut this error by a factor of 2-5.
Sam
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There are two simple ways:
a) use ground based radar and tell the probe where it is - that is classic
b) use astro navigation, drawback is you need a camera or some antenna to lock on pulsars etc. - also classic
I guess the idea to use GPS is based on the fact that GPS receivers are a commodity now ... every (smart)phone has one.
It's all talk, we're never going back (Score:2)
Otherwise we would be there now.
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Otherwise we would be there now.
Based on what. Why would we be there? What would we be doing there? You go to places to do a thing. You need to have a reason to go somewhere and plan to get there.
It's like me saying it was all talk that I was going to drive to Germany 4 weeks ago and I'm never going because I wasn't there, completely ignoring that my car was in the workshop.
Your logic ... isn't logic.
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It's like me saying it was all talk that I was going to drive to Germany 4 weeks ago and I'm never going because I wasn't there,
I isn't "we" as much as one isn't many. Singular and plural nouns have a function. We is referring to the human race. You are not the human race.
Your logic ... isn't logic.
You criticize my logic with such an obvious flaw in your own logic.
completely ignoring that my car was in the workshop.
If your car was in the workshop for longer than it took to build the car in the first place you would question sincerity of the multiple excuses given for the delays.
Otherwise we would be there now.
Based on what. Why would we be there? What would we be doing there? You go to places to do a thing. You need to have a reason to go somewhere and plan to get there.
We have had ample industrial capacity to go back to the moon for decades. I personally believe there are reasons to go back to th
Just put up a GPS around the Moon (Score:3)
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Reddit has some interesting writeups related to this
Starlink solution to GPS denied environments [reddit.com]
What is the cost of an atomic clock? [reddit.com]
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Starlinks are in much lower orbits than GPS satellites, and have a correspondingly shorter lifetime.
The original (and replacement) PGS satellites were deployed 2 or 3 to a launch. The more recent replacements 3 or 4 to a launch. You might get a dozen to a Starlink-a-like launch, and still need 5 or so launches.
to put them into lunar orbits ... you'd be lucky to get 2 per launch (at my guess). you've go
Don't bother (Score:2)
Since NASA's moon rocket is years behind and way over budget, Musk will use one of his own rockets to place 60 GPS Satellites around the moon before landing there.
Precision (Score:2)
"position in space to within 200 to 300 meters"
I'd hate to miss the LM on the other side of a hill by that margin while the oxygen supply of my backpack is running out...
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If you have been so stupid as to put yourself in that sort of position (by not following the "thirds" rule), than you deserve your fatal re-education, and any offspring you have also deserve to die (or minimally, be publicly sterilised) for your error. you're a dangerous failure, and the species is better with you and your genes dead.
Question on details (Score:2)
Are the signals from the GPS satellites omnidirectional? I don't know where to look at the specs but I am pretty sure they optimize their energy over the disc of the Earth from their point of view. From the pictures those are directional antennas.
So if that is right that means that if you are on the surface of the moon you could have line-of-sight to a GPS satellite that you can't get a signal from. You are more likely to get a signal from a much further satellite that appears closer to the Earth's
Re: Question on details (Score:1)
Dilution of Precision (Score:2)
Re: Dilution of Precision (Score:1)
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The GPS-based landing system prototypes we were building in the '80s depended on using multiple overhead SVs. (Testing was tricky because the constellation wasn't even fully populated yet.) You want more to be seeing more SVs that are more overhead---you'll have larger PDOP (from larger HDOP) but you don't care about that so much. Lowering VDOP is your goal when knowing your altitude is important. True, your overall positioning accuracy is better when tracking a widely spread selection of SVs but the config
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Which is why I suggested putting a GPS-class satellite at L4 and L5, to give at least one signal from a substantially different distance to the rest.
Putting one at L2 would help considerably too. More than one at L1
GNSS in LEO, GEO and Beyond (Score:3)
A while back I participated in a study into using GNSS (GPS, BeiDou, Galileo, etc.) with SmallSats in LEO. We got a basic simulator running that showed the signal processing changes needed (mainly increased Doppler compensation), and were done.
Then we got curious and started raising the orbit. We could get good fixes all the way out to GEO, but once above the GNSS constellations (generally located in MEO) most of the antennas are pointed away, so we had to use some tricks to get more "satellites in view", such as using signals bounced from oceans.
We then increased antenna gain so we could use these fainter signals, only to find that we became able to see some fixed terrestrial beacons! This let us push the simulation all the way out to lunar orbit, including the lunar Lagrange points.
To further improve the signal, we simulated GNSS satellites at the lunar Lagrange points (all but L3). This could work! But it would likely prove far more practical to have just one at L1, then a separate lunar constellation.
Here comes the first crater crash... (Score:2)
But why? (Score:1)
The Apollo missions got to the moon and back just fine with gyroscopes and the DKSY flight computer/ground station tracking long before there was a such thing as GPS.
This is a solution looking for a problem.
Unlock code (Score:1)
Turn on your GPS. Detects you're on the moon. Comes up:
Congratulation, you're on the moon. Please enter in your code to unlock Moon Mode.
Let the jokes begin.
The G is for "Global". Duh. (Score:1)
The G is for "Global". The moon is a globe.
Of course it'll work. Duh.
It's science!