3
$\begingroup$

I would like to know, what is the most sophisticated or preferred approach when it comes to connecting a "low earth orbit satellite" to a "low power transmitter devices on the ground".

I know there are various factors to it, ranging from antenna design to access channel design to receiver configuration. But I am novice in the technologies to choose to make it one system and the flow that should happen to have an efficient uplink communication from ground to the satellite.

If someone who has worked on it can give an idea on this considering the fact that "Ground devices are low power", it would be a lot of help.

Improve this question
$\endgroup$
1
  • 2
    $\begingroup$ Consider dropping by at Amateur Radio. Despite the "amateur" in the name, amateur radio can be approached quite professionaly, and many radio amateurs actually work in relevant fields. There are even amateur radio satellites! Getting an amateur radio license would allow you to experiment with radio, which might help you get a feel for these things. $\endgroup$
    – user
    Commented Jun 16, 2017 at 18:31

1 Answer 1

Reset to default
4
$\begingroup$

This is long, but it's still barely scratching the surface. I'll try to take it nice and slow, so bear with me.

Generally, when dealing with radio links, it's a good idea to start with a link budget.

In a link budget, you start with your transmitter's output power, end with the signal strength actually received (most often, this is the minimum required signal strength at the receiver), and in between, list all factors that contribute to either loss or gain of signal strength. This can be everything from antenna gain to attenuation because of absorption in the atmosphere.

Very broadly speaking, there are three ways you can increase signal strength:

  • either by pumping more power into the transmit-side antenna,
  • or by having a bigger antenna at the transmit side,
  • or by having a bigger antenna at the receive side,

or of course some combination of those.

"Bigger antennas" is a bit of a misnomer, but it's close enough to get a basic understanding of what's involved physically. What you really use in such a case is an antenna with a higher antenna gain.

In radio, one often refers to an "isotropic" antenna. This is a purely theoretical construct, which cannot exist in the real world, but which is said to radiate equally in every direction, and to radiate exactly 100% of the power it receives in the form of radio signals. In physics terms, it's a RF point source. Real-world antennas can then be compared to such a theoretical antenna.

When an antenna focuses the signal in some particular direction, it accepts the same amount of power but transmits (or receives) that power in a narrower beam than the isotropic antenna does. We call that "antenna gain", but it's important to keep in mind that there is no actual gain involved; except for losses (which are typically resistive or inductive), the same amount of power is always involved. An antenna can even legitimately have negative gain compared to an isotropic antenna, but such cases are not relevant here. Look at a satellite dish, or a rooftop TV antenna; those are two different types of the general class of directional antennas, so called because they concentrate the power into a beam that is much narrower than that of an isotropic antenna. For spacecraft that travel far from Earth, bigger parabolic antennas (like that satellite TV dish) is used; for a real-world example of this, consider the ground stations for NASA's Deep Space Network.

There is, of course, one more option. Instead of simply pumping more power into the antenna, you can design your signal encoding in such a way that it can be decoded at a lower received power. Very often, this involves reducing the transmission bit rate. Basically, when each bit ("symbol") is allowed more time, the receiver has more time to determine its value, and it can use this time to metaphorically dig the signal out of the noise. The ultimate limit to this is described by the Shannon–Hartley theorem.

Given all this, we can see what can be done given your constraints.

One side of the link (the satellite) is in low Earth orbit, and the other side of the link is on the ground. Thus there is little that can be done about the distance that needs to be covered by the signal.

The frequency needs to be relatively high, so that antennas are physically smaller, because things that are sent into space need to fit inside the spacecraft that are used to launch them. Unfortunately, this means that the signal losses over a given physical path are larger, because free-space path loss scales with distance in terms of wavelengths, and wavelength is the reciprocal of frequency. Thankfully, physical antenna sizes go down with frequency, so we can compensate for this.

The transmitted power level is low. This means that we need to be able to pick out and decode a signal that may be close to, or possibly even below, the ambient noise level at the frequency in use. This benefits from long signal integration times, which reduces our attainable symbol rate. Thankfully, this is a good thing for the power budget of the satellite; you can get away with less on-board power generation capability, and need less cooling. (Believe it or not, but getting rid of waste heat is one of the hardest things in spacecraft design. Reducing excess weight is another.)

Assuming that a low bit rate is acceptable, we can choose the signal encoding such that the required received power level is attainable given the other constraints. This is good, because we really don't have much left to play with!

All this means that you would want to pick a frequency that is as high as reasonably possible (while avoiding the atmospheric absorption bands, for example that of water around 2.3 to 2.4 GHz or so) to get more antenna gain with a same-physical-size antenna, and put a relatively large antenna on the satellite in order to listen in the direction of the Earth without listening to too much else. The physical size of the antenna and the frequency would probably be selected together, such that the area seen by the satellite's antenna is no larger than the Earth itself in its intended orbit, and might be smaller. You would choose a signal encoding that ensures that the signal can be decoded at the received power you would be seeing, with a good deal of margin for loss of signal strength. Hopefully you don't need to transmit a lot of data in a short period of time; if you do, you might have to go back to the drawing board.

All of those factors (frequency, antenna type and size, signal encoding, bit rate) affect each other, so you would be choosing them together. If one of them is fixed (for example, the physically largest dimension of the satellite will be restricted by, if nothing else, the payload fairing of the chosen launcher), then something else has to give.

Improve this answer
$\endgroup$
7
  • $\begingroup$ "The frequency needs to be relatively high...the signal losses over a given physical path are larger, because free-space path loss scales with distance in terms of wavelengths..." I'm not sure this is the best wording. There are different sources of atmospheric absorption&scatter at different wavelengths, but I think you're referring to the definition of a 0 dB gain receiving antenna having an effective area of one square wavelength. The derivation takes the ratio of that area over the area of the sphere $4 \pi R^2$ but it's not really a wavelength-dependent signal loss over a physical path. $\endgroup$
    – uhoh
    Commented Jun 16, 2017 at 23:27
  • $\begingroup$ Thanks for the answer. I calculated path loss and got a value of around 28 dB. That is ok. But what i want to know is how does the number of transmitters on the ground and the very low power they serve, will affect the receiver ? How can we design the receiver for the said constraints? Is there some special theory which needs to be considered in this case? $\endgroup$
    – 14yearoldprogrammer
    Commented Jun 17, 2017 at 14:17
  • $\begingroup$ @uhoh Check the linked question on link budgets. The only non-constant factor in the free space path loss equation is $\frac{r}{\lambda}$ where $r$ is physical distance and $\lambda$ is wavelength, so free space path loss scales with distance in wavelengths. Since wavelength is the reciprocal of frequency, if you change the frequency, the distance in terms of wavelengths changes as the inverse of the change of frequency. Given a distance in terms of wavelengths, the free space path loss is constant regardless of wavelength. Ignoring a bundle of things for simplicity, of course. $\endgroup$
    – user
    Commented Jun 17, 2017 at 15:29
  • 1
    $\begingroup$ @14yearoldprogrammer 28 dB path loss from Earth surface to LEO at any reasonable frequency sounds exceptionally low. (I'd expect on the order of 100 dB. The difference between ~30 dB and ~100 dB is seven orders of magnitude: 10,000,000 times more or less signal.) I'm willing to bet that you made a mistake somewhere. To begin with, double-check your units. $\endgroup$
    – user
    Commented Jun 17, 2017 at 15:31
  • $\begingroup$ @MichaelKjörling I know it's written that way, but the intensity at a distance is really $1/r^2$ in Watts/m^2. The effective cross-sectional area of a 0dB gain antenna is $1 \lambda^2$, so the power received happens to be proportional to $(\lambda/r)^2$. But it's not like different wavelengths loose different amounts of power over a given distance. Algebraically the lambda just gets stuffed inside the parentheses. The link budget formalism is a horrible, evil construct. I call it "dB's for dummies" because it allows people to get the answer without necessarily understanding why it works. $\endgroup$
    – uhoh
    Commented Jun 17, 2017 at 16:55

Your Answer

By clicking “Post Your Answer”, you agree to our terms of service and acknowledge you have read our privacy policy.

Not the answer you're looking for? Browse other questions tagged or ask your own question.