Maneuver Trim

Maneuver Trim is a flight control system state within the broader category of trim conditions, distinguished by its specific equilibrium configuration during accelerated flight maneuvers, wherein aerodynamic, propulsive, and inertial forces and moments are balanced to maintain a desired non-steady, non-level flight path.

6

Publications

323

Citations

63

Authors

23

Institutions

Publications per year

2017–2026

0

Authors

63

  1. DE
    Daniella E. Raveh

    Technion – Israel Institute of Technology, Israel

    2 publications · 89 citations

    2

    h-index

  2. SO
    Shoko Ohtsuki

    Japan Aerospace Exploration Agency, Japan

    1 publications · 124 citations

    1

    h-index

  3. TS
    Takehiko Satoh

    Institute of Space and Astronautical Science, Japan

    1 publications · 124 citations

    1

    h-index

  4. RN
    Ryosuke Nakamura

    National Institute of Advanced Industrial Science and Technology, Japan

    1 publications · 124 citations

    1

    h-index

  5. YK
    Yukio Kamata

    Japan Aerospace Exploration Agency, Japan

    1 publications · 124 citations

    1

    h-index

1–5 of 63

Venues

  1. Journal of Aircraft

    2 publications · 89 citations

    2

    h-index

  2. 1

    h-index

  3. Journal of Guidance Control and Dynamics

    1 publications · 63 citations

    1

    h-index

  4. AIAA Journal

    1 publications · 29 citations

    1

    h-index

  5. Earth Planets and Space

    1 publications · 124 citations

    1

    h-index

1–5