Rendezvous Trajectory Design

Rendezvous Trajectory Design is a specialized method within spacecraft trajectory design that involves the systematic planning and optimization of a chaser spacecraft's path to safely and efficiently approach and meet a target spacecraft in orbit, distinguishing itself by incorporating relative motion dynamics, proximity operations constraints, and mission-specific objectives such as fuel minimization or time of flight.

152

Publications

5.1K

Citations

389

Authors

127

Institutions

Publications per year

2017–2026

54

Authors

389

  1. KC
    Kathleen C. Howell

    Purdue University West Lafayette, United States

    5 publications · 144 citations

    5

    h-index

  2. YL
    Ya-Zhong Luo

    National University of Defense Technology, China

    5 publications · 169 citations

    5

    h-index

  3. BD
    Bernd Dachwald

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    4 publications · 177 citations

    4

    h-index

  4. AA
    Alessandro A. Quarta

    University of Pisa, Italy

    4 publications · 133 citations

    4

    h-index

  5. RW
    Robert W. Farquhar

    Johns Hopkins University Applied Physics Laboratory, United States

    3 publications · 65 citations

    3

    h-index

1–5 of 389

Venues

  1. Journal of Guidance Control and Dynamics

    23 publications · 1.3K citations

    20

    h-index

  2. Acta Astronautica

    22 publications · 677 citations

    18

    h-index

  3. Journal of Spacecraft and Rockets

    17 publications · 528 citations

    12

    h-index

  4. Aerospace Science and Technology

    AST · 10 publications · 284 citations

    10

    h-index

  5. Advances in Space Research

    6 publications · 151 citations

    6

    h-index

1–5