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Constellation Satellite Design - Science topic

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how far can i take gravity assist manoeuvre and how it works?
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Thank you very much @mustafa kamil
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Dear all, I'd like to open here a sort of forum for understanding how the geodesists community is moving in view of the X-band SAR satellite constellation. The new constellation will offer new "free, near real-time SAR data" with the "latest information about any spot on the planet within the hour". This will open completely new horizons for InSAR monitoring of ground deformation especially for rapid phenomena such as eruptions and seismic crises. The huge amount of so frequent data acquisitions will open also new needs for rapid and automatic processing. My question are: who knows more? Are you planning a routine use of these data? How?
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"Capella makes a portion of its historical archived imagery available through the Open Data Program".
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Hello. I am trying to understand which is the minimum revisit time for precision agriculture purposes. I am aware that each crop and each physical parameter in the crop requires different revisit time, but if you could adress me to some paper or work that explains how they select the revisit time for at least one parameter in a crop, I would be gratefull. (Just to specify, I am referring to revisit time of a satellite). Thanks. Let me know if I wasn't clear enough.
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Vittorio Sartoretto It has to do with the dynamics of target variable, let's say leaf biomass / LAI. Within each variable you will get crop and variety variability. And also seasonal variability. I guess it is to difficult to give generic values. Once you have the crop, the variety and the variable defined then you need to get hold (sampling) of key points in the curve order to describe it.
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When creating a scenario in order to analyze a link budget in the case of ISL, what would be the given criteria to stablish Tx gain, Rx gain, Power transmitted and the rest of the system parameters for a given link between two satellites in different orbit planes?
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It is better to use any text book related to the satellite communication.Go in detail and the after all ,it would be easy to consider some additional parameter( attenuation due to weather/ foliage etc) apart from basics as your have considered previously such power, frequency,polarisation,height,gain etc.
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I'm looking for information on the size of the global satellite industry - both commercial and whatever information is available on government. I'd like to know more about the number of satellites in the various orbits, number of geosynchronous satellites, construction and launch cost data, and potential future uses.
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Euroconsult's report
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My aim is to design a LEO constellation to have regional cover.The number of satellite is 12 so my network has inter satellite link sometimes. But I do not know the typical frequency that ISL works at. And how to calculate the ISL budget. The other question is how can I simulate ISL and which software is useful? 
Thanks
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To begin, you'll also need to state how many planes, what the separation of those planes will be and how many satellites are in each plane.
Typically, purpose built communications between satellites is colloquially called "Crosslink". As this is outside the atmosphere your only limiting factors are: 1) Free Space Path Loss 2) Inter-spacecraft network knowledge; how aware does each satellite have to be about where it is in the constellation 3) pointing and directionality of your crosslink. 4) How much money you have to get all this done? 5) ITU available frequencies.
It can take up to 4 years to get the okay from ITU to use a given frequency. Not including the orbital slot. No, I have not filed ITU paperwork myself. The U of M is still building and iterating on its nanosatellite communications boards.
The software package you're looking for is called the Systems Tool Kit (STK) from Analytical Graphics Inc. (AGI)
With it you can model the orbits, the figure of merit for coverage over an area and the link budget. Optimising the orbits using the Walker tool is a non-trival process. They do have a tools called Analyzer and Optimizer that streamline the process. But they aren't free. You'll need some fun justification to your department for those costs. 
You can apply to get and educational licence here:
They also have excellent training guides:
The alternative software solution for you is called FreeFlyer from a.i. solutions.
So far I haven't had any experience with FreeFlyer. I'd love to give it a try to see how and why it differs from STK.
Be aware that currently, satellite systems technology is often under ITARS restriction from the U.S. and as such your institution may not have access to all of the available features.
Here's a random ITU link for the Space Services Department
You've got a great deal of study ahead of you. The learning curve is steep. 
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When I move all pixel linearly computer vision optical flow method doesn't give linear movement of all pixel. Example, when I shift all pixel in [10  10]. It doesn't give me correct answer for all pixel.
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You most likely are facing the so-called aperture problem, which is typically caused by the lack of (or too regular a) texture in the limited scope of the given image; consider using the normal flow, which could produce a more stable solution. 
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All (according to my knowledge) GPS satellite planning software calculate satellite number and DOP's in one point (position). Do you know any software solution for constellation planning along the line (for example - 50 km of railroad) which is passed (for example - 5 hours)?
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1. Download "ORBITRON" (free s/w tool available @http://www.stoff.pl/) and run it.
2. Update TLE files for operational GPS from http://celestrak.com/NORAD/elements/gps-ops.txt
3. Use simulation utility of orbitron with your updated location --> jump intervals of time to simulate the GPS constellation for future times (or location)
4. For a suitable point of time (may be each 30 minutes), select a GPS satellite on the right hand bottom "skyplot" window
5. When a satellite is selected - click on "ROTOR/RADIO" tab --> you can note the elevation and azimuth of each satellite --> Note down the elevation and azimuth of all GPS satellites (above the cut off mask) for this particular point of time.
6. You can use any DOP calculating s/w for each point (of time OR location)
7. We have developed a program to do the same that calculates PDOP values fairly accurately from elevation and azimuth of satellites, please let me know if you need support.
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I want to model a NGEO satellite constellation with terrestrial networks so i need to know some routing algorithms.
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Routing algorithms depends on the application. In case of satellite constellation you can take advantage of the ciclic change of the topologies. In data networks, as Internet, the problem is bonded different, links can appear or disappear in any time, therefore they are not predictable. If you would know about these protocols, try to search with their names; for instance, to wired networks you have OSPF, RIP, and BGP, and for ad-hoc networks good exponents are AODV, OLSR, BATMAN.
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SCIAMACHY which is onboard the Envisat has 3 different modes of measurements. (link : http://www.iup.uni-bremen.de/sciamachy/instrument/modes/index.html) . In Nadir it is easy to understand that location is beneath the sensor. But in limb or occultation mode if we consider some measurements what location does they belong to (in the sense geo-location of the measurement) as the measurements here are tangent to atmosphere.
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For SCIAMACHY limb measurements, see e.g. this paper:
Accounting for the effect of horizontal gradients in limb measurements of scattered sunlight
J. Puķīte, S. Kühl, T. Deutschmann, U. Platt, and T. Wagner
Atmos. Chem. Phys., 8, 3045-3060, 2008
We hope to publish a paper soon that contains a discussion on the effects of inhomogeneous or "small" aerosol and cloud layers (small in comparison with the instruments field of view) on limb reflectance. I will keep you informed, if you're interested.