Three-axis Stabilization

Three-Axis Stabilization is a spacecraft attitude control method that maintains precise orientation along the roll, pitch, and yaw axes simultaneously by employing feedback control systems and onboard actuators to suppress angular deviations relative to a desired inertial or orbital reference frame.

105

Publications

3.6K

Citations

451

Authors

137

Institutions

Publications per year

2017–2026

24

Variants

Three-axis Attitude Control

Authors

451

  1. WH
    Willem H. Steyn

    Stellenbosch University, South Africa

    4 publications · 159 citations

    4

    h-index

  2. QH
    Qinglei Hu

    Beihang University, China

    4 publications · 287 citations

    4

    h-index

  3. DC
    Dengqing Cao

    Harbin Institute of Technology, China

    4 publications · 152 citations

    4

    h-index

  4. YH
    Y. Hashida

    University of Surrey, United Kingdom

    3 publications · 90 citations

    3

    h-index

  5. MR
    Mahmut Reyhanoglu

    Embry–Riddle Aeronautical University, United States

    3 publications · 80 citations

    3

    h-index

1–5 of 451

Venues

  1. Journal of Guidance Control and Dynamics

    10 publications · 468 citations

    10

    h-index

  2. Acta Astronautica

    7 publications · 259 citations

    7

    h-index

  3. Aerospace Science and Technology

    AST · 5 publications · 107 citations

    4

    h-index

  4. Chinese Journal of Aeronautics

    CJA · 3 publications · 65 citations

    3

    h-index

  5. Chinese Physics B

    2 publications · 30 citations

    2

    h-index

1–5