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Initial orbit determination using multiple observations

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Publication:361668
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DOI10.1007/s10569-010-9321-3zbMath1270.70020OpenAlexW2025474881MaRDI QIDQ361668

Daniele Mortari, Reza Raymond Karimi

Publication date: 30 August 2013

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-010-9321-3

zbMATH Keywords

initial orbit determinationLagrange coefficientsmultiple observationstracking LEO satellites


Mathematics Subject Classification ID

Two-body problems (70F05) Orbital mechanics (70M20)


Related Items

Analytic characterization of measurement uncertainty and initial orbit determination on orbital element representations, Parallel initial orbit determination using angles-only observation pairs



Cites Work

  • Single lunation \(N\)-observation orbits
  • Laplacian orbit determination and differential corrections
  • Dependence on the observational time intervals and domain of convergence of orbital determination methods
  • A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight
  • Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
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This page was last edited on 30 January 2024, at 03:52.
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