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Differential positioning experiment using two geostationary satellites

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3 Author(s)
Ito, K. ; Electron. Navigation Res. Inst., Minist. of Transp., Tokyo, Japan ; Hoshinoo, K. ; Ito, M.

A ranging and positioning system for a ship or an aircraft using two geostationary satellites is described. This system has a ranging and positioning accuracy of 100 m and 1 km. Experiments to estimate this system were performed using a ship in the Pacific Ocean in a normal and a differential modes. This system leads to the development of fundamental ranging and positioning techniques for the cooperated independent surveillance

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Aerospace and Electronic Systems, IEEE Transactions on  (Volume:35 ,  Issue: 3 )