Yaw Coupled Dynamics

Yaw Coupled Dynamics is a dynamic model in flight mechanics that characterizes the lateral-directional motion of an aircraft by explicitly accounting for the aerodynamic and inertial interactions between yaw, roll, and sideslip degrees of freedom.

6

Publications

191

Citations

18

Authors

9

Institutions

Publications per year

2017–2026

1

Authors

18

  1. BC
    Bo Cheng

    Pennsylvania State University, United States

    1 publications · 14 citations

    1

    h-index

  2. YY
    Yang Yan

    Liaocheng University, China

    1 publications · 23 citations

    1

    h-index

  3. MO
    Matko Orsag

    University of Zagreb, Croatia

    1 publications · 108 citations

    1

    h-index

  4. CK
    Christopher Korpela

    Drexel University, United States

    1 publications · 108 citations

    1

    h-index

  5. RL
    Robert Langlois

    Carleton University, Canada

    1 publications · 18 citations

    1

    h-index

1–5 of 18

Venues

  1. Journal of Aircraft

    2 publications · 31 citations

    2

    h-index

  2. 1

    h-index

  3. IET Intelligent Transport Systems

    1 publications · 23 citations

    1

    h-index

1–3