Shape-based Trajectory Optimization

Shape-Based Trajectory Optimization is a trajectory design methodology that belongs to the class of indirect optimization techniques and is distinguished by its use of predefined geometric shapes to parameterize the spacecraft's path, enabling analytical or semi-analytical solutions to boundary value problems in orbital mechanics.

25

Publications

1.1K

Citations

69

Authors

30

Institutions

Publications per year

2017–2026

9

Authors

69

  1. BJ
    Bradley J. Wall

    University of Illinois Urbana-Champaign, United States

    3 publications · 248 citations

    3

    h-index

  2. MH
    Mingying Huo

    Harbin Institute of Technology, China

    3 publications · 49 citations

    3

    h-index

  3. NQ
    Naiming Qi

    Harbin Institute of Technology, China

    3 publications · 49 citations

    3

    h-index

  4. JM
    James M. Longuski

    Purdue University West Lafayette, United States

    3 publications · 327 citations

    3

    h-index

  5. AE
    Anastassios E. Petropoulos

    Jet Propulsion Laboratory, United States

    3 publications · 327 citations

    3

    h-index

1–5 of 69

Venues

  1. Journal of Guidance Control and Dynamics

    5 publications · 378 citations

    5

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 92 citations

    3

    h-index

  3. Advances in Space Research

    2 publications · 38 citations

    2

    h-index

  4. Structural and Multidisciplinary Optimization

    2 publications · 54 citations

    2

    h-index

  5. Journal of Spacecraft and Rockets

    2 publications · 270 citations

    2

    h-index

1–5