State Transition Matrices

State Transition Matrices is a mathematical construct in orbital dynamics that belongs to the class of propagation methods and is distinguished by its role in linearly mapping the perturbed state of a spacecraft's trajectory at one epoch to another, thereby quantifying the sensitivity of the orbit to initial conditions over time.

539

Publications

29.2K

Citations

1.1K

Authors

564

Institutions

Publications per year

2017–2026

101

Authors

1.1K

  1. TL
    Tongliang Liu

    The University of Sydney, Australia

    6 publications · 454 citations

    6

    h-index

  2. BH
    Bo Han

    Hong Kong Baptist University, Hong Kong SAR China

    6 publications · 454 citations

    6

    h-index

  3. MS
    Masashi Sugiyama

    Tokyo Institute of Technology, Japan

    6 publications · 454 citations

    6

    h-index

  4. LC
    Lirong Cui

    Beijing Institute of Technology, China

    5 publications · 165 citations

    5

    h-index

  5. CL
    Chao Luo

    Shandong Normal University, China

    5 publications · 116 citations

    5

    h-index

1–5 of 1.1K

Venues

  1. IEEE Transactions on Automatic Control

    17 publications · 1.6K citations

    15

    h-index

  2. Journal of Guidance Control and Dynamics

    18 publications · 1.7K citations

    15

    h-index

  3. arXiv (Cornell University)

    Repository · 16 publications · 734 citations

    13

    h-index

  4. Journal of Applied Probability

    JAP · 13 publications · 295 citations

    12

    h-index

  5. SSRN Electronic Journal

    Repository · 11 publications · 313 citations

    10

    h-index

1–5