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
Parents
27
1–5 of 27
87
2
h-index
2
h-index
2
h-index
2
h-index
1
h-index
1–5 of 87
43
Johnson Space Center
Houston, United States
4 h-index
5 publications
314 citations

Draper Laboratory
Cambridge, United States
2 h-index
7 publications
121 citations

Beihang University
Beijing, China
2 h-index
5 publications
91 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
2 h-index
9 publications
216 citations

Beijing Institute of Technology
Beijing, China
2 h-index
7 publications
255 citations
Space Research Institute
Graz, Austria
1 h-index
1 publications
11 citations

Chinese Academy of Sciences
Beijing, China
1 h-index
1 publications
25 citations
University of Washington
Seattle, United States
1 h-index
5 publications
140 citations
1–8 of 43
2 publications · 33 citations
2
h-index
2 publications · 43 citations
2
h-index
1 publications · 11 citations
1
h-index
Conference · 1 publications · 23 citations
1
h-index
Conference · 1 publications · 16 citations
1
h-index
1–5