Rotorcraft Trim

Rotorcraft Trim is a dynamic equilibrium condition in which a rotorcraft maintains steady, unaccelerated flight at a constant attitude and velocity with all control inputs and rotor system states held constant.

21

Publications

627

Citations

46

Authors

15

Institutions

Publications per year

2017–2026

4

Authors

46

  1. FG
    Farhan Gandhi

    Pennsylvania State University, United States

    3 publications · 50 citations

    3

    h-index

  2. DA
    David A. Peters

    Washington University in St. Louis, United States

    3 publications · 178 citations

    3

    h-index

  3. MK
    Martin K. Sekula

    Langley Research Center, United States

    2 publications · 35 citations

    2

    h-index

  4. IC
    Inderjit Chopra

    University of Maryland, College Park, United States

    2 publications · 66 citations

    2

    h-index

  5. HY
    Hongrui Yu

    Zhejiang University, China

    1 publications · 13 citations

    1

    h-index

1–5 of 46

Venues

  1. Journal of Aircraft

    6 publications · 136 citations

    6

    h-index

  2. Journal of the American Helicopter Society

    3 publications · 94 citations

    3

    h-index

  3. Journal of Guidance Control and Dynamics

    2 publications · 45 citations

    2

    h-index

  4. AIAA Journal

    1 publications · 19 citations

    1

    h-index

  5. 1

    h-index

1–5