Reaction Wheel Control

Reaction Wheel Control is a spacecraft attitude control method that uses the angular momentum of a spinning flywheel to generate torque for precise orientation adjustments by varying the wheel's rotational speed in response to control commands.

255

Publications

7.7K

Citations

685

Authors

223

Institutions

Publications per year

2017–2026

55

Variants

Reaction Wheel Attitude Control

Authors

685

  1. HS
    Hanspeter Schaub

    University of Colorado Boulder, United States

    8 publications · 302 citations

    8

    h-index

  2. IK
    Ilya Kolmanovsky

    University of Michigan, United States

    7 publications · 237 citations

    7

    h-index

  3. DW
    D. W. Miller

    European Organization for Nuclear Research, Switzerland

    5 publications · 251 citations

    5

    h-index

  4. KY
    Kazuya Yoshida

    Tohoku University, Japan

    5 publications · 109 citations

    5

    h-index

  5. VL
    Vaios Lappas

    University of Surrey, United Kingdom

    4 publications · 132 citations

    4

    h-index

1–5 of 685

Venues

  1. Journal of Guidance Control and Dynamics

    38 publications · 1.5K citations

    22

    h-index

  2. Acta Astronautica

    16 publications · 428 citations

    14

    h-index

  3. AIAA Guidance, Navigation, and Control Conference

    Conference · 7 publications · 91 citations

    7

    h-index

  4. 6

    h-index

  5. AIAA Guidance, Navigation, and Control Conference and Exhibit

    Conference · 6 publications · 210 citations

    6

    h-index

1–5