Elliptic Orbits

Elliptic Orbits is a type of Keplerian orbit characterized by a closed, oval-shaped trajectory with an eccentricity strictly between 0 and 1, arising as a solution to the two-body problem under an inverse-square gravitational force.

261

Publications

9.2K

Citations

479

Authors

273

Institutions

Publications per year

2017–2026

40

Authors

479

  1. SR
    Srinivas R. Vadali

    Texas A&M University, United States

    5 publications · 248 citations

    5

    h-index

  2. PS
    Prasenjit Sengupta

    Texas A&M University, United States

    5 publications · 248 citations

    5

    h-index

  3. AA
    Alessandro A. Quarta

    University of Pisa, Italy

    4 publications · 100 citations

    4

    h-index

  4. RB
    R. Broucke

    The University of Texas at Austin, United States

    4 publications · 556 citations

    4

    h-index

  5. GM
    Giovanni Mengali

    University of Pisa, Italy

    4 publications · 100 citations

    4

    h-index

1–5 of 479

Venues

  1. Journal of Guidance Control and Dynamics

    34 publications · 2K citations

    24

    h-index

  2. Celestial Mechanics and Dynamical Astronomy

    14 publications · 403 citations

    12

    h-index

  3. 12

    h-index

  4. Acta Astronautica

    14 publications · 329 citations

    12

    h-index

  5. AIAA Journal

    10 publications · 624 citations

    10

    h-index

1–5