Fig. 7From: A new approach for cycle slip detection and fix using single GPS receiver’s single satellite dual frequency data containing arbitrarily large pseudorange errorsThe distribution of remaining cycle slip pairs after applying rule two with SIPEmax = 100 m, \( {\mathrm{TECR}}_{\Phi}^{\mathrm{max}}\left(\mathrm{k}\right)=0.15\ \mathrm{TECU}/\mathrm{second} \) and ∆t = 1.0 secondBack to article page