Nonlinear Attitude-orbit Interaction

Nonlinear Attitude-Orbit Interaction is a theoretical framework in astrodynamics that characterizes the bidirectional, nonlinear coupling between a spacecraft's rotational dynamics and its orbital motion, where the attitude evolution induces non-negligible perturbations on the trajectory and vice versa, deviating significantly from decoupled or linearized models.

25

Publications

609

Citations

61

Authors

36

Institutions

Publications per year

2017–2026

9

Variants

Nonlinear Attitude-orbit Coupling

Authors

61

  1. AL
    A.Y.T. Leung

    City University of Hong Kong, Hong Kong SAR China

    2 publications · 58 citations

    2

    h-index

  2. HS
    Hassan Salarieh

    Sharif University of Technology, Iran

    2 publications · 40 citations

    2

    h-index

  3. JK
    Jinlu Kuang

    Nanyang Technological University, Singapore

    2 publications · 58 citations

    2

    h-index

  4. LC
    Li‐Qun Chen

    Shanghai University, China

    2 publications · 33 citations

    2

    h-index

  5. KC
    Kathleen C. Howell

    Purdue University West Lafayette, United States

    2 publications · 60 citations

    2

    h-index

1–5 of 61

Venues

  1. Acta Astronautica

    5 publications · 109 citations

    5

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 94 citations

    3

    h-index

  3. Nonlinear Dynamics

    3 publications · 52 citations

    3

    h-index

  4. Journal of Spacecraft and Rockets

    2 publications · 33 citations

    2

    h-index

  5. Journal of Sound and Vibration

    JSV · 2 publications · 88 citations

    2

    h-index

1–5