Sidereon.OrbitDetermination.OrbitFitSolution (Sidereon v0.18.0)

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Initial-state orbit fit for one satellite.

Summary

Types

t()

Types

t()

@type t() :: %Sidereon.OrbitDetermination.OrbitFitSolution{
  covariance: Sidereon.OrbitDetermination.OrbitFitCovariance.t(),
  fit_rms_3d_m: float(),
  geometry_quality: map(),
  initial_state: map(),
  iterations: non_neg_integer(),
  satellite: String.t(),
  seed_rms_3d_m: float()
}