Transfer Orbit Design

Transfer Orbit Design is a methodological framework within spacecraft trajectory design that specifically governs the formulation and optimization of orbital transfer paths, distinguished by its focus on determining the most efficient trajectory parameters, timing, and maneuver sequences to transition a spacecraft between initial and target orbits while satisfying mission constraints.

12

Publications

284

Citations

30

Authors

15

Institutions

Publications per year

2017–2026

2

Authors

30

  1. DF
    David Folta

    Goddard Space Flight Center, United States

    1 publications · 23 citations

    1

    h-index

  2. WZ
    Wanmeng Zhou

    National University of Defense Technology, China

    1 publications · 33 citations

    1

    h-index

  3. RP
    Ryan P. Russell

    The University of Texas at Austin, United States

    1 publications · 13 citations

    1

    h-index

  4. HL
    Haiyang Li

    National University of Defense Technology, China

    1 publications · 33 citations

    1

    h-index

  5. PC
    Pingyuan Cui

    Beijing Institute of Technology, China

    1 publications · 28 citations

    1

    h-index

1–5 of 30

Venues

  1. Journal of Guidance Control and Dynamics

    2 publications · 46 citations

    2

    h-index

  2. Acta Astronautica

    1 publications · 49 citations

    1

    h-index

  3. Advances in Space Research

    1 publications · 33 citations

    1

    h-index

  4. Science China Technological Sciences

    1 publications · 28 citations

    1

    h-index

  5. 1

    h-index

1–5