Sequential Orbit Determination
Sequential Orbit Determination is a method within the field of orbit determination that processes observational data in a time-sequential manner to iteratively estimate and refine the trajectory of a space object using filtering techniques such as the Kalman filter.
10
Publications
311
Citations
22
Authors
13
Institutions
Publications per year
2017–2026
2
Parents
10
1–5 of 10
22
2
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13
China Astronaut Research and Training Center
Beijing, China
2 h-index
2 publications
27 citations
Tsinghua University
Beijing, China
2 h-index
7 publications
94 citations
Jet Propulsion Laboratory
Pasadena, United States
1 h-index
7 publications
294 citations
Texas A&M University
College Station, United States
1 h-index
2 publications
116 citations
Lockheed Martin (United States)
Bethesda, United States
1 h-index
1 publications
28 citations
Istituto di Scienza e Tecnologie dell'Informazione "Alessandro Faedo"
Pisa, Italy
1 h-index
1 publications
56 citations
Institut national de l’information géographique et forestière
Saint-Mandé, France
1 h-index
1 publications
42 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
1 h-index
1 publications
12 citations
1–8 of 13
2 publications · 27 citations
2
h-index
2 publications · 86 citations
2
h-index
1 publications · 56 citations
1
h-index
1 publications · 20 citations
1
h-index
1 publications · 12 citations
1
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