Trajectory Phasing Analysis

Trajectory Phasing Analysis is a computational method used in interplanetary mission design that determines the optimal timing and orbital geometry for spacecraft departure and arrival to achieve desired trajectory characteristics while minimizing propellant consumption.

6

Publications

109

Citations

22

Authors

8

Institutions

Publications per year

2017–2026

3

Authors

22

  1. RB
    Russell Boyce

    The University of Queensland, Australia

    1 publications · 18 citations

    1

    h-index

  2. MX
    MA Xiaobing

    National University of Defense Technology, China

    1 publications · 14 citations

    1

    h-index

  3. CD
    Christopher D. Hall

    Virginia Tech, United States

    1 publications · 24 citations

    1

    h-index

  4. AG
    Antonio Giannitrapani

    University of Siena, Italy

    1 publications · 11 citations

    1

    h-index

  5. VC
    Victor Collazo-Perez

    Virginia Tech, United States

    1 publications · 24 citations

    1

    h-index

1–5 of 22

Venues

  1. Journal of Guidance Control and Dynamics

    2 publications · 35 citations

    2

    h-index

  2. The Journal of the Astronautical Sciences

    1 publications · 30 citations

    1

    h-index

  3. Acta Astronautica

    1 publications · 14 citations

    1

    h-index

  4. Advances in Space Research

    1 publications · 18 citations

    1

    h-index

  5. Journal of Spacecraft and Rockets

    1 publications · 10 citations

1–5