Launch Vehicle Trajectory Optimization

Launch Vehicle Trajectory Optimization is a computational framework within trajectory optimization that specifically addresses the determination of optimal flight paths for launch vehicles by balancing performance, safety, and vehicle constraints during ascent through atmospheric and orbital regimes.

165

Publications

5.2K

Citations

369

Authors

121

Institutions

Publications per year

2017–2026

40

Authors

369

  1. PL
    Ping Lu

    Iowa State University, United States

    10 publications · 973 citations

    10

    h-index

  2. AC
    Anthony Calise

    Georgia Institute of Technology, United States

    9 publications · 320 citations

    9

    h-index

  3. HL
    He Linshu

    Beihang University, China

    6 publications · 132 citations

    6

    h-index

  4. MS
    Martin Sippel

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    4 publications · 68 citations

    4

    h-index

  5. ZS
    Zhengyu Song

    Beijing Aerospace Flight Control Center, China

    4 publications · 77 citations

    4

    h-index

1–5 of 369

Venues

  1. Journal of Guidance Control and Dynamics

    25 publications · 1.6K citations

    18

    h-index

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

    Conference · 15 publications · 405 citations

    12

    h-index

  3. Aerospace Science and Technology

    AST · 13 publications · 420 citations

    12

    h-index

  4. Acta Astronautica

    13 publications · 327 citations

    12

    h-index

  5. Journal of Spacecraft and Rockets

    6 publications · 148 citations

    6

    h-index

1–5