Page 41 - 卫星导航2021年第1-2合期
P. 41

Du et al. Satell Navig             (2021) 2:3                                            Page 8 of 22





                end (Dach et al. 2006; El-Mowafy et al. 2016). Tey   or ambiguity fxing, and the resultant unreliability of
                are assumed to be constant during short-to-medium   ambiguity fxing (Henkel et al. 2016; Seepersad and
                observing periods, but may vary slowly or abruptly   Bisnath 2015).
                in various situations including receiver or antenna
                replacement, satellite component switching or acti-    Multipath/NLOS  is  environment-dependent  and
                vation, thermal variation of receiver or satellite (dur-  is especially severe in dense urban areas where tall
                ing eclipse season), aging and so on (Imparato et al.   buildings refect, difract and/or block the GNSS sig-
                2018b).                                           nals (Groves et al. 2013; van Nee 1995). Furthermore,
                                                                  low-cost GNSS receivers may sufer from larger mul-
              •  Incorrect phase biases. Tese biases are also fre-  tipath and NLOS errors than geodetic-grade receiv-
                quency-dependent and system-dependent, and are    ers due to their poor multipath/NLOS suppression
                relative  values  (between  satellites  and  receivers).   (Murrian  et  al.  2016; Pesyna  et  al.  2014)  and low-
                Similar to code biases, phase biases are considered   quality antennas, challenging their use in high pre-
                stable, although short-term variations have been   cision positioning for ITS. Terefore, quality control
                observed due to ambient temperature efects (Zhang   and stochastic modelling are very important in PPP
                et al. 2017). In fact, the factors leading to code bias   processing when using low-cost devices (Bisnath
                variations can also afect phase biases. Network gen-  et al. 2018). A comprehensive overview of multipath
                erated phase biases may be either not reliable or not   and NLOS characteristics and their mitigation can be
                fully available due to network-end errors. Mismodel-  found in Imparato et al. (2018b).
                ling of the hardware delay, i.e. biases in the estimated
                UPDs/FCBs, IRCs or DSCs, will be absorbed into the   •  Cycle slips. Tere are fve main causes for cycle
                estimated ambiguity terms, causing incorrect fxed-  slips: signal obstruction, low signal-to-noise ratio,
                PPP solutions, or even failure in ambiguity fxing   receiver software faults (Hofmann-Wellenhof et al.
                (Geng et  al.  2012). Cheng, et  al. (2017) proposed a   2001), receiver dynamics (Julien  2005), and high
                quality control and reliability analysis procedure for   level of ionospheric disturbance (Cai et  al.  2012).
                their own FCB and IRC estimation to achieve reliable   Cycle slips are more likely to occur in dense urban
                PPP-AR. Teir detector for FCB was able to detect   environments, especially for receivers mounted on
                small phase outliers (larger than 0.4 cycles) and the   a moving vehicle. As a result, ITS applications are
                undetectable outliers had insignifcant impact on   easily afected by cycle slips. Cycle slips are a major
                estimated FCBs.                                   challenge for PPP processing for both foat-PPP
                                                                  and PPP-AR solutions. Unfxed or incorrectly fxed
                                                                  cycle slips can result in the need for re-initialisation
                                                                  and reconvergence of ambiguity parameters or lead
            Work environment                                      to incorrect ambiguity estimation. Consequently,
                                                                  the reliability, continuity and availability of the
              •  Multipath and NLOS. Code multipath may cause     navigation system may not meet the performance
                range errors of up to 150  m for L1, while NLOS   requirements of ITS.
                errors can be up to several kilometres (Groves et al.
                2013). Te dual-frequency IF combinations will fur-    A number of algorithms for cycle slip detection and
                ther amplify these efects. Carrier-phase multipath   correction which apply to standalone GNSS position-
                is much lower (about two orders of magnitude) than   ing have been proposed. Real-time dual-frequency
                those of code observations. Te maximum carrier-  cycle slip correction algorithms are typically based
                phase multipath error is frequency-dependent and   on a time-diferenced geometry-free combination
                amounts to 1/4 cycle (Georgiadou and Kleusberg    (Banville et al. 2010; Kim and Langley 2001; Zhang
                1988; Braasch  1992). NLOS carrier-phase error is   and Li 2012). Tis kind of measurement combination
                within half a cycle (modulo one carrier cycle) (Groves   is sensitive to the temporal variation of ionospheric
                et  al.  2013). Since the accuracy of PPP depends on   delay, receiver phase wind-up, and multipath. Tus,
                the carrier-phase observations, the impact of code   ionospheric variations and other parameters should
                multipath on PPP can be down weighted and is not   be  estimated along with  the integer  cycle slips. In
                as severe as that for code-only positioning tech-  addition, an integer validation procedure is needed to
                niques. Te major adverse efect of code multipath is   determine the correct number of integer cycle slips
                the longer time needed for the solution convergence   (Zhang and Li 2016).
   36   37   38   39   40   41   42   43   44   45   46