Optimal Multiple-Impulse Direct Ascent Fixed-Time Rendezvous

DOI10.2514/3.49376zbMath0293.70020OpenAlexW2048159419MaRDI QIDQ4045720

John E. Prussing, Larry R. Gross

Publication date: 1974

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.49376

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (7)

Applications of celestial mechanics in natural objects and spacecrafts ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Station keeping of constellations using multiobjective strategies ⋮ Robust tracking control for rendezvous in near-circular orbits ⋮ An analytical description of the three-dimensional swing-by ⋮ Celestial mechanics, spacecrafts, and 50th years of the first humans on the Moon ⋮ Optimal impulsive ellipse-to-circle coplanar rendezvous

This page was built for publication: Optimal Multiple-Impulse Direct Ascent Fixed-Time Rendezvous