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





            anywhere in the world (Zumberge et al. 1997). However,   aviation cannot be applied directly for ITS applications
            PPP can also be augmented by a regional reference sta-  due to diferent requirements and the challenging urban
            tion network or integrated with SBAS services (Heßel-  environment (Zhu et al. 2018). Moreover, considering the
            barth and Wanninger 2013; Wübbena et al. 2005). Hence   diferent types of observations and models of positioning
            PPP is more fexible than the diferential GNSS position-  techniques, it is especially difcult to provide integrity
            ing techniques, making it an attractive technique for   for PPP users.
            many precise positioning applications. With the devel-  Knowledge of the characteristics of PPP vulnerabilities
            opment of new GNSS signals, new GNSS constellations,   and  their mitigation  methods  is  essential to  improving
            and infrastructures, PPP with real-time Ambiguity Reso-  the reliability and integrity of PPP. Tis paper extends
            lution (AR) is an attractive alternative to the diferential   the work of Imparato et al. (2018b), which provided an
            GNSS positioning techniques (Collins  2008; Ge et  al.   overview of vulnerabilities in RTK and SBAS. Te goal
            2008; Laurichesse and Mercier  2007). Te advent of   is to review potential faults and threats in GNSS PPP
            dual-frequency mass-market GNSS chipsets with carrier-  as well as the research developments and key issues of
            phase measurement capability further enhances the PPP   PPP integrity monitoring, focusing on the challenges of
            technique for autonomous driving applications (de Groot   its  application  in  ITS.  Section  A  brief  overview  of  PPP
            et  al.  2018; Murrian et  al.  2016; xAUTO technology   characteristics gives a brief introduction to the PPP tech-
            2017). Moreover, the integration of PPP with other tech-  nique, including its concept, models, and implementa-
            nologies, such as an Inertial Navigation System (INS),   tions. Section Vulnerabilities and integrity fault analysis
            can shorten the convergence/reconvergence time of the   in PPP lists the potential failure modes of PPP, with the
            PPP solution and improve the positioning availability,   demonstrations of fault analysis methods and detailed
            making PPP more applicable, even in an urban environ-  discussion of the main vulnerabilities of GNSS PPP. Sec-
            ment (Gao et al. 2017; Zhang and Gao 2008).       tion GNSS integrity concept and approaches reviews the
              One  of  the  key  issues  for  ITS  technology  is  safety,   status of PPP integrity research and identifes some open
            which cannot be assured without reliable and trustwor-  research issues concerned with PPP vulnerabilities and
            thy positioning. However, due to the weak GNSS satellite   integrity, with a focus on urban scenarios. A summary is
            signals, GNSS measurements are vulnerable to a number   given in section Integrity of PPP in ITS context.
            of threats and faults caused by satellites and/or receiver
            problems, as well as the environment, particularly in   A brief overview of PPP characteristics
            urban areas where ITS technology is most in demand   PPP is a high precision positioning technique which can
            (Ioannides et al. 2016; Martins 2014; Tomas et al. 2011).   be performed with a single GNSS receiver, utilising the
            Furthermore, unlike diferential GNSS positioning meth-  undiferenced measurements of both code and carrier-
            ods such as RTK and NRTK, PPP only relies on the meas-  phase. Te PPP technique requires the precise orbit and
            urements from the user receiver. Many error sources,   clock information of satellites (via so-called “data prod-
            such as satellite clock ofsets, initial satellite and receiver   ucts”) to achieve high positioning accuracy. Real-time
            phase biases and so on, cannot be eliminated or mitigated   orbit and clock products are expressed as the correc-
            in  undiferenced  processing (Bisnath and  Gao  2009).   tions to broadcast ephemeris messages and are dissemi-
            As a result, PPP is more afected by such errors. On the   nated  via  the  Internet  or  broadcast  by  satellites  (either
            other hand, the carrier-phase cycle slip and outlier edit-  SBAS or GNSS satellites, in the case of the latter as for
            ing for PPP is more challenging than for the diferen-  the planned High Precision Service of Galileo naviga-
            tial positioning methods (Kouba et  al.  2017). Although   tion satellite system) (Fernandez-Hernandez et al. 2018;
            GNSS threats have been investigated in many studies,   Heßelbarth and Wanninger 2013; the International GNSS
            and monitoring systems are increasingly being deployed   Service (IGS) 2019; Weber et al. 2007). In addition, the
            (Bhatti and Ochieng 2007; Martins 2014; Ochieng et al.   observations are corrected for the errors due to relativ-
            2003; Tomas et al. 2011; Tombre et al. 2017), few refer   ity, satellite and receiver Phase Centre Ofsets (PCO)
            explicitly to the PPP technique.                  and Phase Centre Variations (PCV) (Schmid et al. 2005),
              ITS applications require high levels of integrity, which   phase wind-up (Wu et al. 1993), troposphere (dry com-
            is  one  of  the  most  important  performance  indicators   ponent),  Earth  tides,  ocean  tide loading,  and  various
            (Zhu et al. 2018). Integrity is concerned with how much   hardware delays or biases, using appropriate models.
            we can trust the positioning results in the cases of both   Other error sources including ionospheric efects, mul-
            nominal and faulted conditions. In recent years, the issue   tipath, Non-Line-of-Sight (NLOS) errors, and cycle slips
            of integrity for land transportation and/or high accuracy   remain the most challenging for real-time ITS applica-
            positioning has attracted more attention. However, the   tions. Tese errors contribute to most of the fault inci-
            classical integrity concept and algorithms developed for   dents for the PPP implemented in urban environments.
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