Stability Augmentation Systems

A Stability Augmentation System is a feedback control system that enhances the inherent stability characteristics of an aircraft by automatically adjusting control surface deflections in response to sensed perturbations, thereby improving steady-state and dynamic flight behavior without altering the pilot’s primary command inputs.

52

Publications

1.5K

Citations

145

Authors

56

Institutions

Publications per year

2017–2026

2

Authors

145

  1. JB
    JOHN B. DEMPSTER

    Wichita Clinic, United States

    2 publications · 39 citations

    2

    h-index

  2. MH
    Mohd. Hasan Ali

    University of Memphis, United States

    2 publications · 160 citations

    2

    h-index

  3. RC
    Ronald Choe

    University of Illinois Urbana-Champaign, United States

    2 publications · 72 citations

    2

    h-index

  4. AA
    A. A. Schy

    Langley Research Center, United States

    2 publications · 34 citations

    2

    h-index

  5. JH
    J. H. Wykes

    Rockwell Automation (United States), United States

    2 publications · 46 citations

    2

    h-index

1–5 of 145

Venues

  1. Journal of Guidance Control and Dynamics

    6 publications · 96 citations

    6

    h-index

  2. Journal of Aircraft

    4 publications · 82 citations

    4

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 4 publications · 185 citations

    4

    h-index

  4. The Aeronautical Journal

    4 publications · 101 citations

    4

    h-index

  5. Journal of the American Helicopter Society

    3 publications · 68 citations

    3

    h-index

1–5