Large-angle Slew Dynamics

Large-Angle Slew Dynamics is a computational model in attitude-orbit coupling that characterizes the nonlinear rotational motion of spacecraft during reorientation maneuvers exceeding 90 degrees, distinguishing itself from small-angle approximations by explicitly accounting for inertial, gyroscopic, and orbital perturbation effects across full-range attitude transitions.

18

Publications

618

Citations

40

Authors

19

Institutions

Publications per year

2017–2026

1

Authors

40

  1. SN
    Sahjendra N. Singh

    University of Nevada, Las Vegas, United States

    2 publications · 89 citations

    2

    h-index

  2. GS
    Gurjeet Singh

    University of Michigan, United States

    2 publications · 197 citations

    2

    h-index

  3. PT
    Pierre T. Kabamba

    University of Michigan, United States

    2 publications · 197 citations

    2

    h-index

  4. AK
    Arun K. Banerjee

    Lockheed Martin (United States), United States

    2 publications · 61 citations

    2

    h-index

  5. NH
    N. Harris McClamroch

    University of Michigan, United States

    2 publications · 197 citations

    2

    h-index

1–5 of 40

Venues

  1. Journal of Guidance Control and Dynamics

    6 publications · 375 citations

    6

    h-index

  2. Acta Astronautica

    2 publications · 32 citations

    2

    h-index

  3. International Journal of Systems Science

    1 publications · 16 citations

    1

    h-index

  4. The Aeronautical Journal

    1 publications · 20 citations

    1

    h-index

  5. Aerospace Science and Technology

    AST · 1 publications · 15 citations

    1

    h-index

1–5