Control Derivatives

Control Derivatives is a stability and control analysis construct in aerospace engineering that quantifies the rate of change of aerodynamic forces and moments with respect to control surface deflections, distinguishing it from other stability derivatives by its exclusive dependence on actuated control inputs rather than vehicle state variables.

166

Publications

6K

Citations

336

Authors

129

Institutions

Publications per year

2017–2026

27

Authors

336

  1. KW
    Kenneth W. Iliff

    Armstrong Flight Research Center, United States

    18 publications · 600 citations

    13

    h-index

  2. RE
    Richard E. Maine

    Armstrong Flight Research Center, United States

    8 publications · 300 citations

    8

    h-index

  3. EA
    Eugene A. Morelli

    Langley Research Center, United States

    7 publications · 252 citations

    7

    h-index

  4. MP
    Meir Pachter

    U.S. Air Force Institute of Technology, United States

    5 publications · 310 citations

    5

    h-index

  5. JA
    Jared A. Grauer

    Langley Research Center, United States

    5 publications · 88 citations

    5

    h-index

1–5 of 336

Venues

  1. Journal of Aircraft

    15 publications · 520 citations

    13

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 13 publications · 399 citations

    13

    h-index

  3. Journal of Guidance Control and Dynamics

    14 publications · 846 citations

    12

    h-index

  4. AIAA Atmospheric Flight Mechanics Conference and Exhibit

    Conference · 7 publications · 221 citations

    7

    h-index

  5. 6

    h-index

1–5