Yaw Damping

Yaw Damping is a control mechanism in aircraft flight dynamics that attenuates unwanted yaw oscillations by introducing a stabilizing moment proportional to the rate of yaw, thereby enhancing directional stability.

61

Publications

1.8K

Citations

156

Authors

72

Institutions

Publications per year

2017–2026

18

Authors

156

  1. JA
    J. Ackermann

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    4 publications · 297 citations

    4

    h-index

  2. SS
    Scott Schreck

    National Laboratory of the Rockies, United States

    2 publications · 66 citations

    2

    h-index

  3. SB
    Stefano Bruni

    Politecnico di Milano, Italy

    2 publications · 54 citations

    2

    h-index

  4. NN
    Niels N. Sørensen

    Technical University of Denmark, Denmark

    2 publications · 66 citations

    2

    h-index

  5. AH
    Aleksander Hać

    Aptiv (United States), United States

    2 publications · 51 citations

    2

    h-index

1–5 of 156

Venues

  1. Vehicle System Dynamics

    11 publications · 442 citations

    10

    h-index

  2. Journal of Aircraft

    4 publications · 75 citations

    4

    h-index

  3. 4

    h-index

  4. Journal of Spacecraft and Rockets

    3 publications · 69 citations

    3

    h-index

  5. 3

    h-index

1–5