Boost Phase Dynamics

Boost Phase Dynamics is a theoretical framework within missile flight dynamics that characterizes the motion, propulsion, and control behavior of a missile during the initial powered ascent stage, distinguishing it by its focus on transient aerodynamic forces, thrust vectoring, and fuel consumption effects prior to payload separation.

31

Publications

613

Citations

89

Authors

34

Institutions

Publications per year

2017–2026

6

Authors

89

  1. BJ
    Byung-Eul Jun

    Agency for Defense Development, South Korea

    2 publications · 39 citations

    2

    h-index

  2. YK
    Youdan Kim

    Seoul National University, South Korea

    2 publications · 39 citations

    2

    h-index

  3. OY
    Oleg Yakimenko

    Naval Postgraduate School, United States

    2 publications · 63 citations

    2

    h-index

  4. TK
    T. Kirubarajan

    McMaster University, Canada

    2 publications · 46 citations

    2

    h-index

  5. YB
    Yaakov Bar‐Shalom

    University of Connecticut, United States

    2 publications · 46 citations

    2

    h-index

1–5 of 89

Venues

  1. Journal of Guidance Control and Dynamics

    5 publications · 110 citations

    5

    h-index

  2. Acta Astronautica

    2 publications · 37 citations

    2

    h-index

  3. AIAA Guidance, Navigation and Control Conference and Exhibit

    Conference · 2 publications · 48 citations

    2

    h-index

  4. Defence Technology

    1 publications · 28 citations

    1

    h-index

  5. International Journal of Aeronautical and Space Sciences

    IJASS · 1 publications · 12 citations

    1

    h-index

1–5