Fig. 8


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Navigation solution for the low latitude receiver FAA1 during 6 days on the spring equinox (DoYs 76–79, 2014). Top panel: maximum values of S4 and σIF. Bottom panel: the number of satellites used to compute the navigation solution (divided by 10) is depicted in black. The σϕ values are depicted in red and the 3D position error is depicted in green. Notice that the solution is reset at 0h on each day.

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