Dealing with uncertainties in angles-only initial orbit determination
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Publication:315251
DOI10.1007/S10569-016-9694-ZzbMath1345.70044OpenAlexW2336058341MaRDI QIDQ315251
Renato Zanetti, Roberto Armellin, Pierluigi di Lizia
Publication date: 19 September 2016
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://eprints.soton.ac.uk/392035/1/PaperCelMecV2.pdf
Orbital mechanics (70M20) General models, approaches, and methods in mechanics of particles and systems (70G99)
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Probabilistic data association: the orbit set ⋮ Nonlinear representation of the confidence region of orbits determined on short arcs
Uses Software
Cites Work
- Application of high order expansions of two-point boundary value problems to astrodynamics
- Multiple solutions in preliminary orbit determination from three observations
- Gravity assist space pruning based on differential algebra
- Propagation of large uncertainty sets in orbital dynamics by automatic domain splitting
- 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
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