Nonlinear Trim

Nonlinear Trim is a computational method used in aerospace engineering to determine equilibrium flight conditions by solving nonlinear systems of equations that model aerodynamic, inertial, and propulsive forces, distinguishing it from linearized trim approaches through its fidelity to complex, real-world vehicle dynamics.

24

Publications

550

Citations

53

Authors

23

Institutions

Publications per year

2017–2026

3

Authors

53

  1. DH
    Dewey H. Hodges

    Georgia Institute of Technology, United States

    7 publications · 232 citations

    7

    h-index

  2. PM
    Pezhman Mardanpour

    Florida International University, United States

    6 publications · 158 citations

    6

    h-index

  3. ZS
    Zahra Sotoudeh

    Georgia Institute of Technology, United States

    3 publications · 102 citations

    3

    h-index

  4. NG
    Nathan Graybeal

    Bihrle Applied Research (United States), United States

    2 publications · 94 citations

    2

    h-index

  5. AD
    Avani Daftary

    Indian Institute of Technology Bombay, India

    2 publications · 30 citations

    2

    h-index

1–5 of 53

Venues

  1. Journal of Aircraft

    5 publications · 223 citations

    5

    h-index

  2. AIAA Journal

    3 publications · 48 citations

    3

    h-index

  3. AIAA Atmospheric Flight Mechanics Conference and Exhibit

    Conference · 1 publications · 13 citations

    1

    h-index

  4. Computers & Operations Research

    1 publications · 40 citations

    1

    h-index

  5. AIAA Guidance, Navigation, and Control Conference

    Conference · 1 publications · 13 citations

    1

    h-index

1–5