Flight Envelope Protection

Flight Envelope Protection is a safety-critical control system function within fly-by-wire aircraft that restricts pilot and autopilot commands to prevent the aircraft from exceeding aerodynamic, structural, or operational flight limits defined by the aircraft’s design envelope.

61

Publications

1.7K

Citations

151

Authors

50

Institutions

Publications per year

2017–2026

16

Authors

151

  1. JV
    J. V. R. Prasad

    Georgia Institute of Technology, United States

    7 publications · 199 citations

    7

    h-index

  2. TL
    Thomas Lombaerts

    Ames Research Center, United States

    6 publications · 129 citations

    6

    h-index

  3. JE
    Joost Ellerbroek

    Delft University of Technology, Netherlands

    5 publications · 122 citations

    5

    h-index

  4. GL
    Gertjan Looye

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    5 publications · 116 citations

    5

    h-index

  5. PG
    Petros G. Voulgaris

    University of Illinois Urbana-Champaign, United States

    5 publications · 263 citations

    5

    h-index

1–5 of 151

Venues

  1. Journal of Guidance Control and Dynamics

    9 publications · 334 citations

    9

    h-index

  2. AIAA Guidance, Navigation, and Control Conference

    Conference · 9 publications · 253 citations

    9

    h-index

  3. International Journal of Aeronautical and Space Sciences

    IJASS · 2 publications · 31 citations

    2

    h-index

  4. AIAA Guidance, Navigation, and Control Conference and Exhibit

    Conference · 2 publications · 49 citations

    2

    h-index

  5. IFAC-PapersOnLine

    2 publications · 24 citations

    2

    h-index

1–5