Быстрая оценка минимального расстояния между двумя конфокальными гелиоцентрическими орбитами

DOI10.14498/vsgtu1344zbMath1413.70001OpenAlexW3017257831MaRDI QIDQ4553514

A. E. Derevyanka

Publication date: 30 October 2018

Published in: Вестник Самарского государственного технического университета. Серия Физико-математические науки (Search for Journal in Brave)

Full work available at URL: http://mathnet.ru/eng/vsgtu1344

zbMATH Keywords

celestial mechanicsorbital elementsMOIDpotentially hazardous asteroids

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Two-body problems (70F05) Celestial mechanics (70F15) Orbital mechanics (70M20)

Cites Work

• A numerical method for calculating minimum distance to near Earth objects
• Computing the critical points of the distance function between two Keplerian orbits via rigorous global optimization
• Distance between two arbitrary unperturbed orbits
• An algebraic method to compute the critical points of the distance function between two Keplerian orbits
• On the distance function between two Keplerian elliptic orbits
• An analytic method to determine future close approaches between satellites
• On the minimum distance between two Keplerian orbits with a common focus
• On the Stationary Points of the Squared Distance between Two Ellipses with a Common Focus

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