Flight Path Angle Dynamics

Flight Path Angle Dynamics is a mathematical model in longitudinal flight dynamics that characterizes the time-varying behavior of the angle between the aircraft's velocity vector and the local horizontal plane, distinguishing itself by its focus on the trajectory倾角's evolution during climb, cruise, and descent phases under aerodynamic, propulsive, and gravitational forces.

72

Publications

3K

Citations

167

Authors

72

Institutions

Publications per year

2017–2026

14

Authors

167

  1. MA
    Michael A. Bolender

    United States Air Force Research Laboratory, United States

    5 publications · 822 citations

    5

    h-index

  2. DD
    David Doman

    United States Air Force Research Laboratory, United States

    5 publications · 822 citations

    5

    h-index

  3. AC
    Anthony Calise

    Georgia Institute of Technology, United States

    5 publications · 167 citations

    5

    h-index

  4. AS
    Andrea Serrani

    The Ohio State University, United States

    4 publications · 754 citations

    4

    h-index

  5. YL
    Yong-In Lee

    Agency for Defense Development, South Korea

    3 publications · 128 citations

    4

    h-index

1–5 of 167

Venues

  1. Journal of Guidance Control and Dynamics

    14 publications · 1.1K citations

    11

    h-index

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

    Conference · 4 publications · 161 citations

    4

    h-index

  3. Journal of Aircraft

    4 publications · 89 citations

    4

    h-index

  4. 3

    h-index

  5. AIAA Journal

    3 publications · 244 citations

    3

    h-index

1–5