Powered Flight Trajectory Modeling

Powered Flight Trajectory Modeling is a computational methodology within launch vehicle trajectory analysis that characterizes the ascent phase of a launch vehicle under active propulsion by integrating dynamic equations of motion with thrust, mass depletion, aerodynamic, and gravitational forces to predict time-varying flight path states.

16

Publications

426

Citations

35

Authors

14

Institutions

Publications per year

2017–2026

2

Authors

35

  1. BD
    Burton D. Fried

    University of California, Los Angeles, United States

    3 publications · 76 citations

    3

    h-index

  2. MS
    Michael S. Selig

    University of Illinois Urbana-Champaign, United States

    2 publications · 63 citations

    2

    h-index

  3. PS
    Pritam Sukumar

    University of Illinois Urbana-Champaign, United States

    2 publications · 63 citations

    2

    h-index

  4. AK
    A. K. Ghosh

    Indian Institute of Technology Kanpur, India

    1 publications · 19 citations

    1

    h-index

  5. PK
    Prashant Kumar

    Indian Institute of Technology Kanpur, India

    1 publications · 19 citations

    1

    h-index

1–5 of 35

Venues

  1. Journal of Aircraft

    2 publications · 64 citations

    2

    h-index

  2. Journal of Applied Physics

    2 publications · 51 citations

    2

    h-index

  3. Jet propulsion

    1 publications · 25 citations

    1

    h-index

  4. 1

    h-index

  5. Advances in Space Research

    1 publications · 24 citations

    1

    h-index

1–5