Two-impulse Transfer Orbits

Two-Impulse Transfer Orbits is a spacecraft trajectory optimization method that belongs to the class of orbital transfer techniques and is distinguished by the application of exactly two instantaneous velocity impulses to achieve a fuel-efficient transition between two coplanar circular orbits.

24

Publications

592

Citations

33

Authors

23

Institutions

Publications per year

2017–2026

3

Authors

33

  1. GA
    Gary A. McCue

    Federal Aviation Administration, United States

    3 publications · 63 citations

    3

    h-index

  2. GZ
    Gang Zhang

    Harbin Institute of Technology, China

    2 publications · 28 citations

    2

    h-index

  3. CO
    C. O. Lau

    Jet Propulsion Laboratory, United States

    2 publications · 54 citations

    2

    h-index

  4. RB
    Richard B. Barrar

    University of Oregon, United States

    2 publications · 41 citations

    2

    h-index

  5. DF
    Derek F. Lawden

    University of Canterbury, New Zealand

    2 publications · 27 citations

    2

    h-index

1–5 of 33

Venues

  1. Journal of Guidance Control and Dynamics

    9 publications · 255 citations

    9

    h-index

  2. AIAA Journal

    5 publications · 98 citations

    5

    h-index

  3. ARS journal

    2 publications · 60 citations

    2

    h-index

  4. Optimal Control Applications and Methods

    1 publications · 46 citations

    1

    h-index

  5. Journal of Aerospace Engineering

    1 publications · 14 citations

    1

    h-index

1–5