Aerodynamic Control Effects

Aerodynamic Control Effects is a theoretical construct within aircraft control that characterizes the changes in aerodynamic forces and moments generated by control surface deflections, distinguishing it from other aerodynamic phenomena through its direct causal relationship to the manipulation of flight vehicle attitude and trajectory.

107

Publications

4.6K

Citations

345

Authors

132

Institutions

Publications per year

2017–2026

37

Authors

345

  1. TC
    Thomas Corke

    University of Notre Dame, United States

    3 publications · 223 citations

    3

    h-index

  2. KM
    Kenneth M. Dorsett

    Lockheed Martin (United States), United States

    3 publications · 87 citations

    2

    h-index

  3. HK
    H.-P. Kau

    Technical University of Munich, Germany

    2 publications · 101 citations

    2

    h-index

  4. JS
    Jubaraj Sahu

    DEVCOM Army Research Laboratory, United States

    2 publications · 40 citations

    2

    h-index

  5. UW
    U. Wenger

    Rolls-Royce (Germany), Germany

    2 publications · 101 citations

    2

    h-index

1–5 of 345

Venues

  1. Physics of Fluids

    4 publications · 79 citations

    4

    h-index

  2. Chinese Journal of Aeronautics

    CJA · 3 publications · 89 citations

    3

    h-index

  3. AIAA Journal

    3 publications · 84 citations

    3

    h-index

  4. 3

    h-index

  5. Aerospace Science and Technology

    AST · 3 publications · 144 citations

    3

    h-index

1–5