Trim Condition Analysis

Trim Condition Analysis is a methodological framework within longitudinal flight dynamics that identifies and evaluates steady-state equilibrium conditions of an aircraft’s motion by determining the specific control and state variable settings that balance all forces and moments, thereby enabling stable and unaccelerated flight.

36

Publications

1.1K

Citations

107

Authors

43

Institutions

Publications per year

2017–2026

9

Authors

107

  1. LE
    Lars E. Ericsson

    Lockheed Martin (United States), United States

    3 publications · 59 citations

    3

    h-index

  2. LW
    Ligang Wu

    Harbin Institute of Technology, China

    2 publications · 86 citations

    2

    h-index

  3. HG
    Huijun Gao

    Harbin Institute of Technology, China

    2 publications · 86 citations

    2

    h-index

  4. HL
    Hongyi Li

    Guangdong University of Technology, China

    2 publications · 86 citations

    2

    h-index

  5. XH
    Xiaoxiang Hu

    Xi'an High Tech University, China

    2 publications · 86 citations

    2

    h-index

1–5 of 107

Venues

  1. Journal of Aircraft

    7 publications · 168 citations

    7

    h-index

  2. AIAA Atmospheric Flight Mechanics Conference

    Conference · 2 publications · 31 citations

    2

    h-index

  3. Optimal Control Applications and Methods

    2 publications · 78 citations

    2

    h-index

  4. Journal of Fluids and Structures

    2 publications · 61 citations

    2

    h-index

  5. AIAA SCITECH 2022 Forum

    Conference · 1 publications · 13 citations

    1

    h-index

1–5