Nonlinear Flight Envelope Analysis

Nonlinear Flight Envelope Analysis is a systematic methodology in aerospace engineering that characterizes the full extent of achievable flight conditions by rigorously accounting for nonlinear aerodynamic, inertial, and control coupling effects that cannot be accurately represented through linearized models.

13

Publications

337

Citations

32

Authors

15

Institutions

Publications per year

2017–2026

3

Authors

32

  1. JB
    Jay Brandon

    Langley Research Center, United States

    2 publications · 56 citations

    2

    h-index

  2. EA
    Eugene A. Morelli

    Langley Research Center, United States

    2 publications · 56 citations

    2

    h-index

  3. YL
    Yinghui Li

    Southwest Jiaotong University, China

    2 publications · 29 citations

    2

    h-index

  4. QC
    Qiping Chu

    Delft University of Technology, Netherlands

    1 publications · 26 citations

    1

    h-index

  5. FC
    Frank C. Sanders

    Southern Illinois University Carbondale, United States

    1 publications · 14 citations

    1

    h-index

1–5 of 32

Venues

  1. Journal of Guidance Control and Dynamics

    3 publications · 103 citations

    3

    h-index

  2. Journal of Aircraft

    2 publications · 58 citations

    2

    h-index

  3. AIAA Guidance, Navigation, and Control Conference

    Conference · 2 publications · 81 citations

    2

    h-index

  4. Measurement and Control

    1 publications · 11 citations

    1

    h-index

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

    Conference · 1 publications · 21 citations

    1

    h-index

1–5