Flight Envelope Stability

Flight Envelope Stability is a formal analytical framework within flight dynamics that characterizes the stability of an aircraft across its entire operational range of altitude, airspeed, and load factors by distinguishing stable, neutral, and unstable regions through combined aerodynamic, inertial, and control surface influence.

46

Publications

1.2K

Citations

143

Authors

48

Institutions

Publications per year

2017–2026

11

Authors

143

  1. JV
    J. V. R. Prasad

    Georgia Institute of Technology, United States

    2 publications · 73 citations

    2

    h-index

  2. JT
    John T. Bosworth

    Armstrong Flight Research Center, United States

    2 publications · 39 citations

    2

    h-index

  3. AC
    Anthony Calise

    Georgia Institute of Technology, United States

    2 publications · 72 citations

    2

    h-index

  4. İY
    İlkay Yavrucuk

    Middle East Technical University, Türkiye

    2 publications · 32 citations

    2

    h-index

  5. HG
    Harry G. Kwatny

    Drexel University, United States

    2 publications · 94 citations

    2

    h-index

1–5 of 143

Venues

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

    Conference · 4 publications · 92 citations

    4

    h-index

  2. Journal of Guidance Control and Dynamics

    4 publications · 171 citations

    4

    h-index

  3. The Aeronautical Journal

    3 publications · 74 citations

    3

    h-index

  4. AIAA Guidance, Navigation, and Control Conference

    Conference · 2 publications · 34 citations

    2

    h-index

  5. Journal of the American Helicopter Society

    2 publications · 73 citations

    2

    h-index

1–5