Sideslip Limits

Sideslip Limits is a flight envelope boundary that defines the maximum allowable sideslip angle at which an aircraft can operate without experiencing adverse aerodynamic effects such as loss of control, directional instability, or structural loading.

17

Publications

879

Citations

58

Authors

27

Institutions

Publications per year

2017–2026

4

Authors

58

  1. JY
    Jonathan Y. M. Goh

    Toyota Research Institute

    1 publications · 45 citations

    1

    h-index

  2. AB
    Avinash Balachandran

    Toyota Research Institute

    1 publications · 45 citations

    1

    h-index

  3. LL
    Lu Liu

    Northwestern Polytechnical University, China

    1 publications · 186 citations

    1

    h-index

  4. AT
    Antonio Tota

    Politecnico di Torino, Italy

    1 publications · 88 citations

    1

    h-index

  5. HF
    H. F. Nelson

    Missouri University of Science and Technology, United States

    1 publications · 11 citations

    1

    h-index

1–5 of 58

Venues

  1. Vehicle System Dynamics

    3 publications · 306 citations

    3

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 2 publications · 22 citations

    2

    h-index

  3. IEEE Transactions on Intelligent Vehicles

    ITIVBL · 1 publications · 96 citations

    1

    h-index

  4. Ocean Engineering

    1 publications · 186 citations

    1

    h-index

  5. 31st Aerospace Sciences Meeting

    1 publications · 14 citations

    1

    h-index

1–5