Descent Navigation Systems

Descent Navigation Systems is a specialized guidance framework in aerospace engineering that determines and controls the trajectory of a spacecraft during atmospheric entry by integrating sensor fusion, real-time state estimation, and adaptive algorithms to ensure precise, safe, and autonomous landing.

27

Publications

680

Citations

87

Authors

43

Institutions

Publications per year

2017–2026

4

Authors

87

  1. JK
    Jun’ichiro Kawaguchi

    Japan Aerospace Exploration Agency, Japan

    2 publications · 33 citations

    2

    h-index

  2. SZ
    Shengying Zhu

    Beijing Institute of Technology, China

    2 publications · 79 citations

    2

    h-index

  3. HE
    Heinz Erzberger

    Ames Research Center, United States

    2 publications · 22 citations

    2

    h-index

  4. PC
    Pingyuan Cui

    Beijing Institute of Technology, China

    2 publications · 79 citations

    2

    h-index

  5. AG
    Alessandro Gardi

    RMIT University, Australia

    1 publications · 17 citations

    1

    h-index

1–5 of 87

Venues

  1. Journal of Guidance Control and Dynamics

    2 publications · 33 citations

    2

    h-index

  2. Advances in Space Research

    2 publications · 43 citations

    2

    h-index

  3. Planetary and Space Science

    1 publications · 11 citations

    1

    h-index

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

    Conference · 1 publications · 23 citations

    1

    h-index

  5. AIAA/AAS Astrodynamics Specialist Conference and Exhibit

    Conference · 1 publications · 16 citations

    1

    h-index

1–5