Ascent Trajectory Optimization

Ascent Trajectory Optimization is a computational methodology within launch vehicle trajectory analysis that determines the optimal control and path parameters during the powered ascent phase to minimize fuel consumption, maximize payload delivery, or satisfy mission-specific constraints while adhering to dynamic, aerodynamic, and gravitational forces.

96

Publications

3K

Citations

238

Authors

77

Institutions

Publications per year

2017–2026

28

Authors

238

  1. PL
    Ping Lu

    Iowa State University, United States

    6 publications · 440 citations

    6

    h-index

  2. AC
    Anthony Calise

    Georgia Institute of Technology, United States

    6 publications · 300 citations

    6

    h-index

  3. AZ
    Alessandro Zavoli

    Sapienza University of Rome, Italy

    4 publications · 161 citations

    4

    h-index

  4. GC
    Guido Colasurdo

    Politecnico di Torino, Italy

    4 publications · 156 citations

    4

    h-index

  5. BP
    Binfeng Pan

    Northwestern Polytechnical University, China

    3 publications · 155 citations

    4

    h-index

1–5 of 238

Venues

  1. Journal of Guidance Control and Dynamics

    19 publications · 1.2K citations

    16

    h-index

  2. Aerospace Science and Technology

    AST · 10 publications · 310 citations

    10

    h-index

  3. Journal of Spacecraft and Rockets

    8 publications · 165 citations

    8

    h-index

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

    Conference · 6 publications · 131 citations

    6

    h-index

  5. Acta Astronautica

    3 publications · 92 citations

    4

    h-index

1–5