GEO (SBAS) satellites handling #433
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Hello @ChristopherRabotin, In RINEX, the ephemeris for GEO and Glonass vehicles describe a state vector, not keplerian parameters, and we are expected to propagate this state in time (either backwards or forward) to get the state at the desired instant. r(t) = r(t0) + v(t0) *dt + 1/2 * a(t0) * dt^2 for example, this is how RTKLIB does it. Currently I do not support that interpolation, so I cannot consider any GEO or Glonass vehicles for my navigation processes, and I'm investigating what needs to be done to change that. If I were to instead deploy a Nyx propagator from that reference state, can I expect significant improvements compared to the basic interpolation method ? thanks |
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Hi Guillaume, I assume that Given the |
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I expect the interpolation as it's currently done to be pretty low fidelity and work only for a few hours at most (I've seen interpolation methods work for longer, but they're usually much more details than a quadratic interpolation). In contrast, with Nyx, you can expect the propagation to be valid for many decades.