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
16
Universal Gravity Turn Trajectories
Glen J. Culler, Burton D. Fried · Journal of Applied Physics · 1957 · 28 citations
1–5 of 16
35
3
h-index
2
h-index
2
h-index
1
h-index
1
h-index
1–5 of 35
14
University of Illinois Urbana-Champaign
Urbana, United States
2 h-index
4 publications
126 citations
IBM (Brazil)
São Paulo, Brazil
1 h-index
1 publications
19 citations
Technical Solutions (United States)
Amarillo, United States
1 h-index
1 publications
33 citations

National University of Defense Technology
Changsha, China
1 h-index
5 publications
80 citations

Indian Institute of Science Bangalore
Bengaluru, India
1 h-index
1 publications
16 citations

Ames Research Center
Mountain View, United States
1 h-index
1 publications
12 citations
Indian Space Research Organisation
Bengaluru, India
1 h-index
1 publications
16 citations
RAM Laboratories (United States)
San Diego, United States
1 h-index
1 publications
25 citations
1–8 of 14
2 publications · 64 citations
2
h-index
2 publications · 51 citations
2
h-index
1 publications · 25 citations
1
h-index
1 publications · 16 citations
1
h-index
1 publications · 24 citations
1
h-index
1–5