Stability Derivatives

Stability Derivatives is a mathematical representation of the partial derivatives of aerodynamic forces and moments with respect to changes in flight state variables or control inputs, used to characterize the inherent dynamic stability and control behavior of an aircraft in flight mechanics.

246

Publications

8.3K

Citations

402

Authors

138

Institutions

Publications per year

2017–2026

16

Authors

402

  1. KW
    Kenneth W. Iliff

    Armstrong Flight Research Center, United States

    19 publications · 672 citations

    14

    h-index

  2. RE
    Richard E. Maine

    Armstrong Flight Research Center, United States

    9 publications · 356 citations

    9

    h-index

  3. AC
    Asha Crasta

    International Islamic University Malaysia, Malaysia

    7 publications · 119 citations

    7

    h-index

  4. SA
    Sher Afghan Khan

    International Islamic University Malaysia, Malaysia

    7 publications · 119 citations

    7

    h-index

  5. SN
    Sahjendra N. Singh

    University of Nevada, Las Vegas, United States

    5 publications · 235 citations

    5

    h-index

1–5 of 402

Venues

  1. Journal of Aircraft

    30 publications · 1.1K citations

    21

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 20 publications · 552 citations

    14

    h-index

  3. Journal of Guidance Control and Dynamics

    17 publications · 794 citations

    14

    h-index

  4. NASA STI Repository (National Aeronautics and Space Administration)

    Repository · 9 publications · 276 citations

    9

    h-index

  5. AIAA Journal

    9 publications · 366 citations

    9

    h-index

1–5