Sequential Orbit Determination

Sequential Orbit Determination is a method within the field of orbit determination that processes observational data in a time-sequential manner to iteratively estimate and refine the trajectory of a space object using filtering techniques such as the Kalman filter.

10

Publications

311

Citations

22

Authors

13

Institutions

Publications per year

2017–2026

2

Authors

22

  1. HB
    Hexi Baoyin

    Tsinghua University, China

    2 publications · 27 citations

    2

    h-index

  2. PM
    Pengbin Ma

    China Astronaut Research and Training Center, China

    2 publications · 27 citations

    2

    h-index

  3. FJ
    Fanghua Jiang

    Tsinghua University, China

    2 publications · 27 citations

    2

    h-index

  4. SD
    S. D. Desai

    Jet Propulsion Laboratory, United States

    1 publications · 42 citations

    1

    h-index

  5. JM
    Junshan Mu

    Tsinghua University, China

    1 publications · 13 citations

    1

    h-index

1–5 of 22

Venues

  1. Journal of Navigation

    2 publications · 27 citations

    2

    h-index

  2. Journal of Spacecraft and Rockets

    2 publications · 86 citations

    2

    h-index

  3. Celestial Mechanics and Dynamical Astronomy

    1 publications · 56 citations

    1

    h-index

  4. Journal of Guidance Control and Dynamics

    1 publications · 20 citations

    1

    h-index

  5. Acta Astronautica

    1 publications · 12 citations

    1

    h-index

1–5