Integrated Flight Control Design

Integrated Flight Control Design is a multidisciplinary optimization framework that systematically unifies aerodynamic, structural, and control system models within the aeroelastic design process to simultaneously enhance aircraft performance, stability, and maneuverability through synergistic interaction of flight control laws and elastic airframe behavior.

47

Publications

1.5K

Citations

145

Authors

49

Institutions

Publications per year

2017–2026

9

Authors

145

  1. SG
    Sanjay Garg

    University of South Australia, Australia

    6 publications · 155 citations

    6

    h-index

  2. DG
    Declan G. Bates

    University of Warwick, United Kingdom

    4 publications · 54 citations

    4

    h-index

  3. JH
    John Hodgkinson

    Imperial College London, United Kingdom

    3 publications · 43 citations

    3

    h-index

  4. IP
    Ian Postlethwaite

    University of Leicester, United Kingdom

    3 publications · 39 citations

    3

    h-index

  5. DM
    Duane Mattern

    Glenn Research Center, United States

    2 publications · 26 citations

    2

    h-index

1–5 of 145

Venues

  1. Journal of Guidance Control and Dynamics

    4 publications · 183 citations

    4

    h-index

  2. 3

    h-index

  3. Guidance, Navigation, and Control Conference

    Conference · 2 publications · 72 citations

    2

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 2 publications · 76 citations

    2

    h-index

  5. 2

    h-index

1–5