Coarse Initial Orbit Determination for a Geostationary Satellite Using Single-Epoch GPS Measurements

A practical algorithm is proposed for determining the orbit of a geostationary orbit (GEO) satellite using single-epoch measurements from a Global Positioning System (GPS) receiver under the sparse visibility of the GPS satellites. The algorithm uses three components of a state vector to determine t...

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Detalles Bibliográficos
Autores principales: Kim, Ghangho, Kim, Chongwon, Kee, Changdon
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2015
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4431311/
https://www.ncbi.nlm.nih.gov/pubmed/25835299
http://dx.doi.org/10.3390/s150407878

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4431311/
https://www.ncbi.nlm.nih.gov/pubmed/25835299
http://dx.doi.org/10.3390/s150407878

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