Thrust Vector Control

Thrust Vector Control is a propulsion system mechanism that actively directs the thrust output of a rocket or aircraft engine by altering the direction of the exhaust jet, thereby enabling controlled changes in vehicle trajectory and attitude.

291

Publications

9.7K

Citations

646

Authors

242

Institutions

Publications per year

2017–2026

81

Authors

646

  1. KW
    Kexin Wu

    Zhejiang Sci-Tech University, China

    8 publications · 199 citations

    8

    h-index

  2. PJ
    P. J. Strykowski

    University of Minnesota, United States

    7 publications · 246 citations

    7

    h-index

  3. HD
    Heuy Dong Kim

    Gyeongguk National University, South Korea

    6 publications · 179 citations

    6

    h-index

  4. BG
    Benjamin Gal‐Or

    Technion – Israel Institute of Technology, Israel

    6 publications · 102 citations

    6

    h-index

  5. ML
    Marco Lovera

    Politecnico di Milano, Italy

    5 publications · 191 citations

    5

    h-index

1–5 of 646

Venues

  1. Journal of Guidance Control and Dynamics

    21 publications · 733 citations

    16

    h-index

  2. Journal of Propulsion and Power

    17 publications · 510 citations

    15

    h-index

  3. AIAA Journal

    14 publications · 488 citations

    13

    h-index

  4. Acta Astronautica

    11 publications · 343 citations

    11

    h-index

  5. 10

    h-index

1–5