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Orbit Determination System for Low Earth Orbit SatellitesThe IAI/MBT Precise Orbit Determination system for Low Earth Orbit satellites is presented. The system is based on GPS pesudorange and carrier phase measurements and implements the Reduced Dynamics method. The GPS measurements model, the dynamic model, and the least squares orbit determination are discussed. Results are shown for data from the CHAMP satellite and for simulated data from the ROKAR GPS receiver. In both cases the one sigma 3D position and velocity accuracy is about 0.2 m and 0.5 mm/sec respectively.
Document ID
20080012697
Document Type
Conference Paper
Authors
Elisha, Yossi (Israel Aerospace Industries Ltd. Israel)
Shyldkrot, Haim (Israel Aerospace Industries Ltd. Israel)
Hankin, Maxim (Israel Aerospace Industries Ltd. Israel)
Date Acquired
August 24, 2013
Publication Date
September 24, 2007
Publication Information
Publication: Proceedings of the 20th International Symposium on Space Flight Dynamics
Subject Category
Space Communications, Spacecraft Communications, Command and Tracking
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20080012629Analytic PrimaryProceedings of the 20th International Symposium on Space Flight Dynamics