Spacecraft Vibration Analysis

Spacecraft Vibration Analysis is a computational and experimental methodology within spacecraft structural engineering that characterizes dynamic responses of space vehicles to vibrational loads during launch and operational environments, distinguishing itself by its focus on predicting, mitigating, and validating structural integrity under time-varying inertial forces specific to aerospace missions.

163

Publications

5.2K

Citations

411

Authors

132

Institutions

Publications per year

2017–2026

35

Authors

411

  1. GS
    Guglielmo S. Aglietti

    University of Southampton, United Kingdom

    7 publications · 256 citations

    7

    h-index

  2. CD
    Conor D. Johnson

    Moog CSA Engineering (United States), United States

    4 publications · 79 citations

    4

    h-index

  3. LM
    L. Meirovitch

    Virginia Tech, United States

    4 publications · 218 citations

    4

    h-index

  4. DC
    Dengqing Cao

    Harbin Institute of Technology, China

    4 publications · 125 citations

    4

    h-index

  5. PS
    Paul S. Wilke

    Moog CSA Engineering (United States), United States

    4 publications · 79 citations

    4

    h-index

1–5 of 411

Venues

  1. Journal of Spacecraft and Rockets

    39 publications · 1.2K citations

    19

    h-index

  2. Journal of Guidance Control and Dynamics

    15 publications · 918 citations

    14

    h-index

  3. Acta Astronautica

    12 publications · 471 citations

    12

    h-index

  4. AIAA Journal

    11 publications · 440 citations

    10

    h-index

  5. Aerospace Science and Technology

    AST · 8 publications · 213 citations

    8

    h-index

1–5