Capture Trajectories

"Capture Trajectory" is a conic section orbit that represents a two-body orbital motion solution wherein a spacecraft approaches a celestial body along a hyperbolic trajectory and employs a maneuver or natural perturbation to transition into a bounded elliptical orbit, distinguishing it from other transfer or flyby trajectories by achieving orbital capture.

56

Publications

1.8K

Citations

121

Authors

57

Institutions

Publications per year

2017–2026

13

Authors

121

  1. JM
    James M. Longuski

    Purdue University West Lafayette, United States

    4 publications · 101 citations

    4

    h-index

  2. RP
    Ryan P. Russell

    The University of Texas at Austin, United States

    3 publications · 72 citations

    3

    h-index

  3. AE
    Alfred E. Lynam

    Purdue University West Lafayette, United States

    3 publications · 77 citations

    3

    h-index

  4. DJ
    Daniel J. Scheeres

    University of Colorado Boulder, United States

    3 publications · 98 citations

    3

    h-index

  5. AF
    A. F. B. A. Prado

    Instituto Nacional de Pesquisas Espaciais, Brazil

    1 publications · 29 citations

    2

    h-index

1–5 of 121

Venues

  1. Journal of Guidance Control and Dynamics

    13 publications · 376 citations

    12

    h-index

  2. Celestial Mechanics and Dynamical Astronomy

    5 publications · 134 citations

    5

    h-index

  3. Acta Astronautica

    4 publications · 144 citations

    4

    h-index

  4. Advances in Space Research

    2 publications · 40 citations

    3

    h-index

  5. The Journal of the Astronautical Sciences

    2 publications · 69 citations

    2

    h-index

1–5