Control Coupling

Control Coupling is a static aeroelastic phenomenon in aircraft stability wherein the deformation of the airframe under aerodynamic loads induces unintended changes in control surface effectiveness or aircraft response, thereby coupling otherwise independent control inputs to rigid-body motions.

67

Publications

3K

Citations

175

Authors

80

Institutions

Publications per year

2017–2026

28

Authors

175

  1. YF
    Yongchun Fang

    Nankai University, China

    6 publications · 414 citations

    7

    h-index

  2. NS
    Ning Sun

    Nankai University, China

    5 publications · 390 citations

    5

    h-index

  3. XL
    Xiao Liang

    Nankai University, China

    1 publications · 101 citations

    2

    h-index

  4. PZ
    Pengcheng Zhu

    Huazhong University of Science and Technology, China

    2 publications · 24 citations

    2

    h-index

  5. XH
    Xiongxiong He

    Zhejiang University of Technology, China

    2 publications · 82 citations

    2

    h-index

1–5 of 175

Venues

  1. Journal of Guidance Control and Dynamics

    4 publications · 366 citations

    4

    h-index

  2. IEEE/ASME Transactions on Mechatronics

    4 publications · 283 citations

    4

    h-index

  3. 2

    h-index

  4. IET Control Theory and Applications

    2 publications · 52 citations

    2

    h-index

  5. Mechatronics

    2 publications · 82 citations

    2

    h-index

1–5