Orbit determination with the two-body integrals. II

DOI10.1007/s10569-011-9357-zzbMath1270.70017arXiv1101.4569OpenAlexW3100379518MaRDI QIDQ362683

Giovanni Federico Gronchi, Davide Farnocchia, Linda Dimare

Publication date: 30 August 2013

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

Full work available at URL: https://arxiv.org/abs/1101.4569

zbMATH Keywords

polynomial equationsKepler problemorbit determinationlinkageattributablesLaplace-Lenz vector

Mathematics Subject Classification ID

Two-body problems (70F05)

Related Items (3)

Optimal starters for solving the elliptic Kepler's equation ⋮ Keplerian integrals, elimination theory and identification of very short arcs in a large database of optical observations ⋮ Orbit determination with the two-body integrals. III

Uses Software

• na10

Cites Work

• Circular and zero-inclination solutions for optical observations of Earth-orbiting objects
• Orbit determination with the two-body integrals
• Numerical computation of polynomial zeros by means of Aberth's method
• Orbit determination of space debris: admissible regions
• Innovative methods of correlation and orbit determination for space debris
• Non-integrability of the problem of motion around an oblate planet
• Theory of Orbit Determination
• On the Stationary Points of the Squared Distance between Two Ellipses with a Common Focus

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