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

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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Bibliográfalaš dieđut
Váldodahkkit: Ghangho Kim, Chongwon Kim, Changdon Kee
Materiálatiipa: Artihkal
Giella:English
Almmustuhtton: MDPI AG 2015-04-01
Ráidu:Sensors
Fáttát:
GEO
GPS
initial state
orbit determination
EKF
space GPS receiver
Liŋkkat:http://www.mdpi.com/1424-8220/15/4/7878

Interneahtta

http://www.mdpi.com/1424-8220/15/4/7878

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