Time-optimal Trajectory Design

Time-Optimal Trajectory Design is a trajectory optimization framework within launch vehicle mission analysis that, as the nearest class, formulates ascent or orbital transfer paths as a mathematical problem of minimizing flight time, and, as the distinguishing characteristic, incorporates dynamic constraints, boundary conditions, and performance limits specific to launch vehicles to achieve the shortest feasible time-to-target while satisfying mission and physical feasibility requirements.

105

Publications

4.5K

Citations

284

Authors

134

Institutions

Publications per year

2017–2026

43

Authors

284

  1. RZ
    Rui Zhang

    National University of Singapore, Singapore

    4 publications · 481 citations

    4

    h-index

  2. YZ
    Yong Zeng

    Southeast University, China

    3 publications · 470 citations

    3

    h-index

  3. ZS
    Zvi Shiller

    University of California, Los Angeles, United States

    3 publications · 115 citations

    3

    h-index

  4. SM
    S.B. Moon

    Purdue University West Lafayette, United States

    2 publications · 38 citations

    2

    h-index

  5. SA
    S. Ahmad

    Purdue University West Lafayette, United States

    2 publications · 38 citations

    2

    h-index

1–5 of 284

Venues

  1. Journal of Guidance Control and Dynamics

    9 publications · 291 citations

    9

    h-index

  2. 4

    h-index

  3. arXiv (Cornell University)

    Repository · 3 publications · 40 citations

    3

    h-index

  4. IEEE Transactions on Industrial Electronics

    2 publications · 92 citations

    2

    h-index

  5. The International Journal of Robotics Research

    IJRR · 2 publications · 262 citations

    2

    h-index

1–5