Active Attitude Control

Active Attitude Control is a control methodology within the domain of spacecraft attitude dynamics that employs powered actuators and real-time feedback to deliberately alter and stabilize the orientation of a spacecraft, distinguishing it from passive or natural stabilization techniques by its reliance on continuous energy input and active intervention.

94

Publications

4K

Citations

250

Authors

107

Institutions

Publications per year

2017–2026

33

Authors

250

  1. QH
    Qinglei Hu

    Beihang University, China

    4 publications · 381 citations

    4

    h-index

  2. SD
    S. Di Gennaro

    University of L'Aquila, Italy

    3 publications · 133 citations

    3

    h-index

  3. JZ
    Jing Zhang

    Beihang University, China

    2 publications · 41 citations

    2

    h-index

  4. AK
    Arun K. Misra

    McGill University, Canada

    2 publications · 30 citations

    2

    h-index

  5. WS
    Walter Santiago

    Glenn Research Center, United States

    2 publications · 45 citations

    2

    h-index

1–5 of 250

Venues

  1. Journal of Guidance Control and Dynamics

    8 publications · 568 citations

    8

    h-index

  2. Aerospace Science and Technology

    AST · 7 publications · 531 citations

    7

    h-index

  3. Acta Astronautica

    7 publications · 193 citations

    7

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 41 citations

    3

    h-index

  5. Journal of Spacecraft and Rockets

    3 publications · 52 citations

    3

    h-index

1–5