Entry Trajectory Design

Entry Trajectory Design is a computational methodology within aerospace engineering that determines the optimal path and control profile for a spacecraft or entry vehicle during atmospheric entry, distinguishing itself from other mission design components by focusing specifically on the vehicle's flight trajectory from atmospheric interface to terminal phase, subject to constraints such as thermal loading, aerodynamic forces, and target accuracy.

112

Publications

4.3K

Citations

261

Authors

74

Institutions

Publications per year

2017–2026

31

Authors

261

  1. PL
    Ping Lu

    Iowa State University, United States

    10 publications · 674 citations

    10

    h-index

  2. GT
    Guojian Tang

    National University of Defense Technology, China

    8 publications · 376 citations

    8

    h-index

  3. LL
    Luhua Liu

    National University of Defense Technology, China

    6 publications · 284 citations

    6

    h-index

  4. KD
    Kenneth D. Mease

    University of California, Irvine, United States

    6 publications · 433 citations

    6

    h-index

  5. WB
    Weimin Bao

    China Aerospace Science and Technology Corporation, China

    6 publications · 213 citations

    6

    h-index

1–5 of 261

Venues

  1. Journal of Guidance Control and Dynamics

    15 publications · 1K citations

    14

    h-index

  2. Journal of Spacecraft and Rockets

    13 publications · 601 citations

    11

    h-index

  3. Aerospace Science and Technology

    AST · 11 publications · 560 citations

    11

    h-index

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

    Conference · 10 publications · 300 citations

    10

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 5 publications · 157 citations

    5

    h-index

1–5