Orbit Design

Orbit Design is a methodological framework within astrodynamics that specifies the construction and optimization of trajectories for spacecraft positioned at or near Lagrange points, distinguished by its integration of gravitational equilibrium conditions and orbital stability constraints inherent to the circular restricted three-body problem.

371

Publications

13.2K

Citations

1.2K

Authors

343

Institutions

Publications per year

2017–2026

80

Authors

1.2K

  1. CR
    Colin R. McInnes

    University of Strathclyde, United Kingdom

    16 publications · 825 citations

    16

    h-index

  2. KC
    Kathleen C. Howell

    Purdue University West Lafayette, United States

    11 publications · 450 citations

    11

    h-index

  3. RP
    Ryan P. Russell

    The University of Texas at Austin, United States

    9 publications · 251 citations

    9

    h-index

  4. DJ
    Daniel J. Scheeres

    University of Colorado Boulder, United States

    5 publications · 160 citations

    5

    h-index

  5. HB
    Hexi Baoyin

    Tsinghua University, China

    5 publications · 253 citations

    5

    h-index

1–5 of 1.2K

Venues

  1. Journal of Spacecraft and Rockets

    50 publications · 1.6K citations

    23

    h-index

  2. Journal of Guidance Control and Dynamics

    32 publications · 1.1K citations

    21

    h-index

  3. Acta Astronautica

    31 publications · 968 citations

    20

    h-index

  4. Advances in Space Research

    19 publications · 503 citations

    14

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 13 publications · 296 citations

    11

    h-index

1–5