Linearized Missile Models

Linearized Missile Models is a mathematical modeling approach in missile flight dynamics that approximates the nonlinear equations of motion through linearization about a steady-state operating point, enabling tractable stability and control analysis using linear system theory.

56

Publications

2K

Citations

115

Authors

49

Institutions

Publications per year

2017–2026

6

Authors

115

  1. JS
    J. Shinar

    Technion – Israel Institute of Technology, Israel

    6 publications · 268 citations

    6

    h-index

  2. TS
    Tal Shima

    Technion – Israel Institute of Technology, Israel

    4 publications · 334 citations

    4

    h-index

  3. SG
    S. Gutman

    Technion – Israel Institute of Technology, Israel

    3 publications · 133 citations

    3

    h-index

  4. MM
    M.C. Mickle

    Louisiana State University, United States

    2 publications · 53 citations

    2

    h-index

  5. DW
    David W. Casbeer

    United States Air Force Research Laboratory, United States

    2 publications · 196 citations

    2

    h-index

1–5 of 115

Venues

  1. Journal of Guidance Control and Dynamics

    15 publications · 769 citations

    14

    h-index

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

    Conference · 2 publications · 61 citations

    2

    h-index

  3. AIAA Guidance, Navigation and Control Conference and Exhibit

    Conference · 2 publications · 39 citations

    2

    h-index

  4. Journal of Guidance and Control

    2 publications · 93 citations

    2

    h-index

  5. Journal of Spacecraft and Rockets

    2 publications · 36 citations

    2

    h-index

1–5