Minimum-energy Transfers

Minimum-Energy Transfers is a spacecraft trajectory optimization method that belongs to the class of orbital transfer strategies and is distinguished by its exploitation of the Hohmann transfer principle to achieve the lowest possible energy expenditure when transitioning between two coplanar circular orbits under two-body dynamics.

25

Publications

936

Citations

58

Authors

40

Institutions

Publications per year

2017–2026

6

Variants

Minimum Energy Transfers

Authors

58

  1. JD
    James D. Biggs

    Politecnico di Milano, Italy

    2 publications · 27 citations

    2

    h-index

  2. DM
    D. Michael McFarland

    University of Illinois Urbana-Champaign, United States

    2 publications · 385 citations

    2

    h-index

  3. AF
    A. F. B. A. Prado

    Instituto Nacional de Pesquisas Espaciais, Brazil

    2 publications · 25 citations

    2

    h-index

  4. FN
    F. Nucera

    University of Reggio Calabria, Italy

    2 publications · 385 citations

    2

    h-index

  5. GF
    Gary Flandro

    University of Tennessee at Knoxville, United States

    1 publications · 10 citations

    1

    h-index

1–5 of 58

Venues

  1. Acta Astronautica

    4 publications · 83 citations

    4

    h-index

  2. Journal of Guidance Control and Dynamics

    3 publications · 43 citations

    3

    h-index

  3. Celestial Mechanics and Dynamical Astronomy

    2 publications · 39 citations

    2

    h-index

  4. Cosmic Research

    2 publications · 25 citations

    2

    h-index

  5. Nonlinear Dynamics

    2 publications · 379 citations

    2

    h-index

1–5