Optimal Orbit Transfer

Optimal Orbit Transfer is a spacecraft trajectory maneuver that belongs to the class of orbital transfer strategies, distinguished by its minimization of propellant consumption or delta-v requirement between two coplanar circular orbits under the two-body assumption.

113

Publications

4.1K

Citations

171

Authors

96

Institutions

Publications per year

2017–2026

13

Authors

171

  1. AA
    Alessandro A. Quarta

    University of Pisa, Italy

    6 publications · 129 citations

    6

    h-index

  2. JA
    Jean Albert Kéchichian

    The Aerospace Corporation, United States

    5 publications · 111 citations

    5

    h-index

  3. TN
    T. N. Edelbaum

    United Aircraft (Russia), Russia

    4 publications · 171 citations

    4

    h-index

  4. CR
    Colin R. McInnes

    University of Strathclyde, United Kingdom

    4 publications · 134 citations

    4

    h-index

  5. GM
    Giovanni Mengali

    University of Pisa, Italy

    4 publications · 104 citations

    4

    h-index

1–5 of 171

Venues

  1. Journal of Guidance Control and Dynamics

    35 publications · 1.4K citations

    23

    h-index

  2. Acta Astronautica

    5 publications · 169 citations

    6

    h-index

  3. Journal of Spacecraft and Rockets

    6 publications · 325 citations

    6

    h-index

  4. AIAA Journal

    6 publications · 169 citations

    6

    h-index

  5. The Journal of the Astronautical Sciences

    5 publications · 154 citations

    5

    h-index

1–5