Distance between two arbitrary unperturbed orbits

DOI10.1007/s10569-004-3207-1zbMath1151.70320OpenAlexW2031479464MaRDI QIDQ815663

Roman V. Baluyev, Konstantin Vladislavovich Kholshevnikov

Publication date: 20 February 2006

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

Full work available at URL: https://doi.org/10.1007/s10569-004-3207-1

zbMATH Keywords

ellipticcritical pointsparabolicdistance functionhyperbolic and rectilinear orbits

Mathematics Subject Classification ID

Celestial mechanics (70F15)

Related Items (9)

Быстрая оценка минимального расстояния между двумя конфокальными гелиоцентрическими орбитами ⋮ Revisiting the computation of the critical points of the Keplerian distance ⋮ Computing the critical points of the distance function between two Keplerian orbits via rigorous global optimization ⋮ Collision criterion for two satellites on Keplerian orbits ⋮ Distance in the space of energetically bounded Keplerian orbits ⋮ Euler configurations and quasi-polynomial systems ⋮ On the distance between two ellipses in \(\mathbb{R}^3\) ⋮ Rigorous Global Optimization for Collision Risk Assessment on Perturbed Orbits ⋮ An algebraic method to compute the critical points of the distance function between two Keplerian orbits

Cites Work

• On the distance function between two Keplerian elliptic orbits
• On the minimum distance between two Keplerian orbits with a common focus
• Unnamed Item

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