Two-body Orbit Dynamics

Two-Body Orbit Dynamics is a mathematical model in orbital mechanics that describes the motion of a spacecraft or celestial body under the influence of gravitational attraction from a single primary body, assuming no perturbations from other forces or bodies.

17

Publications

1.8K

Citations

47

Authors

40

Institutions

Publications per year

2017–2026

6

Authors

47

  1. EI
    Elbaz I. Abouelmagd

    National Research Institute of Astronomy and Geophysics, Egypt

    1 publications · 14 citations

    1

    h-index

  2. GD
    G. Djurašević

    Astronomical Observatory, Serbia

    1 publications · 15 citations

    1

    h-index

  3. HA
    H. Ak

    Ankara University, Türkiye

    1 publications · 15 citations

    1

    h-index

  4. BA
    B. Albayrak

    Ankara University, Türkiye

    1 publications · 15 citations

    1

    h-index

  5. SE
    S. Erkapić

    Astronomical Observatory, Serbia

    1 publications · 15 citations

    1

    h-index

1–5 of 47

Venues

  1. Journal of Guidance Control and Dynamics

    2 publications · 42 citations

    2

    h-index

  2. Celestial Mechanics and Dynamical Astronomy

    2 publications · 69 citations

    2

    h-index

  3. 2

    h-index

  4. Icarus

    1 publications · 32 citations

    1

    h-index

  5. A&A

    1 publications · 16 citations

    1

    h-index

1–5