Sun-pointing Dynamics

Sun-Pointing Dynamics is a control-theoretic framework within attitude-orbit coupling that governs the orientation and orbital motion of a spacecraft to maintain a fixed alignment with the Sun, distinguished by its integration of solar vector referencing with coupled rotational and translational dynamics for precision pointing and orbit stabilization.

35

Publications

1.5K

Citations

109

Authors

39

Institutions

Publications per year

2017–2026

9

Authors

109

  1. AA
    Alessandro A. Quarta

    University of Pisa, Italy

    3 publications · 62 citations

    3

    h-index

  2. GM
    Giovanni Mengali

    University of Pisa, Italy

    3 publications · 62 citations

    3

    h-index

  3. TS
    Takanao Saiki

    Japan Aerospace Exploration Agency, Japan

    2 publications · 45 citations

    2

    h-index

  4. AJ
    Alan J. Laub

    University of California, Santa Barbara, United States

    2 publications · 28 citations

    2

    h-index

  5. JL
    Junfeng Li

    Tsinghua University, China

    2 publications · 56 citations

    2

    h-index

1–5 of 109

Venues

  1. Journal of Guidance Control and Dynamics

    5 publications · 445 citations

    5

    h-index

  2. Acta Astronautica

    4 publications · 149 citations

    4

    h-index

  3. Advances in Space Research

    3 publications · 68 citations

    3

    h-index

  4. Energy Conversion and Management

    2 publications · 314 citations

    2

    h-index

  5. ANU Open Research (Australian National University)

    Repository · 2 publications · 24 citations

    2

    h-index

1–5