Inertial Pointing

Inertial Pointing is a spacecraft attitude control strategy that maintains orientation relative to an inertial reference frame by minimizing angular drift with respect to fixed celestial coordinates, distinguishing it from Earth-referenced or body-fixed pointing techniques.

13

Publications

486

Citations

28

Authors

13

Institutions

Publications per year

2017–2026

2

Authors

28

  1. ML
    Marco Lovera

    Politecnico di Milano, Italy

    4 publications · 179 citations

    4

    h-index

  2. AA
    Alessandro Astolfi

    Imperial College London, United Kingdom

    3 publications · 129 citations

    3

    h-index

  3. FD
    Fabrice Delhaye

    Safran (France), France

    1 publications · 32 citations

    1

    h-index

  4. MS
    Mike Soutullo

    Teledyne Technologies (United States), United States

    1 publications · 39 citations

    1

    h-index

  5. MW
    Mark Whorton

    Marshall Space Flight Center, United States

    1 publications · 39 citations

    1

    h-index

1–5 of 28

Venues

  1. Journal of Guidance Control and Dynamics

    4 publications · 160 citations

    4

    h-index

  2. 1

    h-index

  3. 1

    h-index

  4. Gyroscopy and Navigation

    1 publications · 32 citations

    1

    h-index

  5. 1

    h-index

1–5