Orbital maneuver optimization using time-explicit power series

DOI10.1007/S10569-011-9336-4zbMath1270.70076OpenAlexW2101773071MaRDI QIDQ362656

James D. Thorne

Publication date: 30 August 2013

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

Full work available at URL: https://doi.org/10.1007/s10569-011-9336-4

zbMATH Keywords

Lambert problemorbital maneuver optimizationorbital mission planningThorne series solution of Lambert problem

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Cites Work

• Unnamed Item
• Application of high order expansions of two-point boundary value problems to astrodynamics
• A procedure for the solution of Lambert's orbital boundary-value problem
• Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.

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