Time-optimal Rendezvous

Time-Optimal Rendezvous is a spacecraft trajectory optimization method that belongs to the class of orbital rendezvous strategies and is distinguished by its objective of minimizing the total time required for a chaser vehicle to intercept and dock with a target spacecraft under dynamic constraints and control limitations.

21

Publications

809

Citations

47

Authors

28

Institutions

Publications per year

2017–2026

5

Authors

47

  1. JE
    John E. Prussing

    University of Illinois Urbana-Champaign, United States

    3 publications · 255 citations

    3

    h-index

  2. AR
    Ariel Rosenfeld

    Bar-Ilan University, Israel

    2 publications · 27 citations

    2

    h-index

  3. RW
    Richard Weber

    University of Cambridge, United Kingdom

    2 publications · 182 citations

    2

    h-index

  4. DW
    Di Wu

    Tsinghua University, China

    2 publications · 34 citations

    2

    h-index

  5. FJ
    Fanghua Jiang

    Tsinghua University, China

    2 publications · 33 citations

    2

    h-index

1–5 of 47

Venues

  1. Journal of Guidance Control and Dynamics

    5 publications · 347 citations

    5

    h-index

  2. Journal of Applied Probability

    JAP · 2 publications · 182 citations

    2

    h-index

  3. Journal of Aerospace Engineering

    1 publications · 12 citations

    1

    h-index

  4. Acta Mechanica Sinica

    1 publications · 12 citations

    1

    h-index

  5. IEEE Transactions on Automatic Control

    1 publications · 17 citations

    1

    h-index

1–5