@inproceedings{57a896d8468e4012be7cf79aebcb0494,
title = "Space trajectory optimization: Differential evolution redux",
abstract = "A modified version of the differential evolution (DE) algorithm, using a hyper-torus for the solution space and an additive component for some of the trial solutions, is applied to two trajectory optimization problems (determining initial conditions for Lyapunov orbits in the circular-restricted three-body problem, and determining optimal steering strategies for a two-arc low-thrust orbital transfer). The results are compared with those using particle swarm optimization (PSO), with DE showing significantly less likelihood of stagnation than PSO, while requiring a modest increase in computation time.",
author = "Melton, {Robert G.}",
year = "2020",
month = jan,
day = "1",
language = "English (US)",
isbn = "9780877036630",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "281--295",
editor = "Razoumny, {Yury N.} and Filippo Graziani and Guerman, {Anna D.} and Jean-Michel Contant",
booktitle = "1st IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials, 2018",
address = "United States",
note = "1st IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials, 2018 ; Conference date: 13-11-2018 Through 15-11-2018",
}