Closed-loop Trajectory Guidance

Closed-Loop Trajectory Guidance is a launch vehicle trajectory guidance method that continuously adjusts the vehicle's flight path in real time by feeding measured state variables into a guidance algorithm to minimize deviations from the desired trajectory.

67

Publications

2.5K

Citations

171

Authors

71

Institutions

Publications per year

2017–2026

17

Authors

171

  1. PL
    Ping Lu

    Iowa State University, United States

    7 publications · 518 citations

    7

    h-index

  2. YK
    Youdan Kim

    Seoul National University, South Korea

    2 publications · 54 citations

    2

    h-index

  3. DL
    Defu Lin

    Beijing Institute of Technology, China

    2 publications · 78 citations

    2

    h-index

  4. RW
    Randal W. Beard

    Brigham Young University, United States

    2 publications · 178 citations

    2

    h-index

  5. CW
    Christopher W. Brunner

    Iowa State University, United States

    2 publications · 113 citations

    2

    h-index

1–5 of 171

Venues

  1. Journal of Guidance Control and Dynamics

    14 publications · 830 citations

    14

    h-index

  2. Aerospace Science and Technology

    AST · 7 publications · 338 citations

    7

    h-index

  3. 5

    h-index

  4. Nonlinear Dynamics

    3 publications · 207 citations

    3

    h-index

  5. AIAA Guidance, Navigation and Control Conference and Exhibit

    Conference · 3 publications · 42 citations

    3

    h-index

1–5