Control Derivative Analysis

Control Derivative Analysis is a methodological framework in linearized flight dynamics that characterizes the sensitivity of aerodynamic forces and moments to control surface deflections by quantifying the partial derivatives of these outputs with respect to control inputs under small-perturbation assumptions.

22

Publications

557

Citations

48

Authors

17

Institutions

Publications per year

2017–2026

2

Authors

48

  1. KW
    Kenneth W. Iliff

    Armstrong Flight Research Center, United States

    7 publications · 116 citations

    7

    h-index

  2. RE
    Richard E. Maine

    Armstrong Flight Research Center, United States

    6 publications · 137 citations

    6

    h-index

  3. MF
    Mary F. Shafer

    Armstrong Flight Research Center, United States

    2 publications · 36 citations

    2

    h-index

  4. DE
    D. E. Stepner

    Systems Control (United States), United States

    2 publications · 56 citations

    2

    h-index

  5. RM
    R.К. Mehra

    Scientific Systems (United States), United States

    2 publications · 56 citations

    2

    h-index

1–5 of 48

Venues

  1. NASA Technical Reports Server (NASA)

    Repository · 5 publications · 118 citations

    5

    h-index

  2. Journal of Aircraft

    2 publications · 66 citations

    2

    h-index

  3. Journal of Guidance Control and Dynamics

    2 publications · 44 citations

    2

    h-index

  4. Shock and Vibration

    1 publications · 14 citations

    1

    h-index

  5. 1

    h-index

1–5