Spacecraft intercept using minimum control energy and wait time

DOI10.1007/s10569-012-9448-5zbMath1266.70043OpenAlexW2045367001MaRDI QIDQ2376766

H. Leeghim

Publication date: 24 June 2013

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

Full work available at URL: https://doi.org/10.1007/s10569-012-9448-5

zbMATH Keywords

orbit transferminimum energyLambert problemnon-coplanar elliptical orbitstwo-impulse rendezvous

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (1)

Autonomous spacecraft rendezvous with finite time convergence

Cites Work

• Unnamed Item
• Optimal two-impulse rendezvous using constrained multiple-revolution Lambert solutions
• A new approach to impulsive rendezvous near circular orbit
• Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
• An elegant Lambert algorithm
• Optimal multiple-impulse time-fixed rendezvous between circular orbits
• Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.

This page was built for publication: Spacecraft intercept using minimum control energy and wait time