|
|
| (7 intermediate revisions by 4 users not shown) |
| Line 1: |
Line 1: |
| {{Article Infobox2 | | {{Article Infobox2 |
| |Category=Fundamentals | | |Category=Fundamentals |
| |Authors=J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. | | |Authors=GMV |
| |Level=Basic | | |Level=Basic |
| |YearOfPublication=2011 | | |YearOfPublication=2013 |
| |Logo=gAGE | | |Logo=GMV |
| |Title={{PAGENAME}} | | |Title={{PAGENAME}} |
| }} | | }} |
| ==Introduction==
| | As of 2011, the SoL service is being re-profiled, one of the solutions under assessment being [[ARAIM]]. |
| Galileo will provide to its users not only a global positioning service, but also the associated integrity information for SoL! (SoL!) services. This is an important contribution of Galileo against the GPS or GLONASS systems, where the SoL! integrity must provided by augmentation systems (WAAS, EGNOS...). Thanks to integrity, the users are constantly aware of whether transmitted signals can be trusted; receiving timely alert messages in case of failures and data to compute the integrity risk for the decision to start a critical operation.
| |
|
| |
|
| The Galileo Ground Segment monitors the Signal-in-Space (SIS) using the measurements of the Galileo Sensor Stations (GSS) network and computes the range error (SIS Error, SISE)<ref group="footnote">Associated to navigation message (ephemeris, clock...)</ref> in real-time, from the known coordinates of satellites and network receivers. It is assumed that, in fault free conditions, a non-biased Gaussian distribution overbonds the SISE at any user location (i.e., SISE is over- bounded by N(0,SISA)). The minimum standard deviation of such Gaussian is called as Signal-In-Space-Accuracy (SISA), see figure 1, left. This expected a-priory accuracy SISA value is similar to the GPS User Range Error (URE), and is broadcasted in the Navigation message with maximum update period of 30 seconds.
| |
|
| |
|
| The Ground System computes also an estimate of the true SISE (eSISE) at the worst location, assuming that the difference between the true and the estimated values (SISE-eSISE) is overbounded by a non-biased Gaussian distribution with standard deviation called SIS Monitoring Accuracy SISMA (i.e., SISE-eSISE is overbounded by N(0,SISMA)), see figure 1, right. Notice that in this context, the SISMA can be considered as a quality measure of the integrity check whiting the Integrity Processing Facility (IPF) [Oehler et al., 2005].
| |
|
| |
|
| The Integrity Processing Facility (IPF) of Galileo Ground segment is comparing in real-time the eSISE with a threshold T. When the eSISE is larger than this threshold<ref group="footnote">It is assumed that the estimated eSISE is also overbounded by <math>N(0,\,\sqrt{SISA^2\, +\, SISMA^2}),\, thence\, T\, =\, K_{pfa} \sqrt{SISA^2\, +\, SISMA^2}</math>, with K<sub>pfa</sub> defined according to the specified false alarm probability. <math>Thence,\, if(eSISE\, >\, T)\, ⇒\, IF\, =\, Not\, −\, OK.</math></ref>, the Integrity Flag (IF) for the SIS associated satellite is set to Not OK. The SISMA value and IF are broadcasted in the Integrity Message for all satellites every 30 seconds. Alerts can be transmitted in real-time (1-second) if required.
| |
| A Galileo user receiver computes its integrity risk at the Alarm Limit (AL) at any global location, combining horizontal and vertical errors and considering both the fault-free and the faulty situation, but with only one failing satellite, and assuming ([Hernandez Mendel et al., 2008], [Oehler et al., 2005]):
| |
| * In Fault-free mode: SISE is overbounded by N(0,SISA).
| |
| * In general the faulty satellites are detected by IPF and flagged as Not-OK.
| |
| * In case of a faulty satellite not detected by IPF (Faulty mode), SISE is overbounded by N(T,SISMA), where T is the IPF rejection threshold of faulty satellites<ref group="footnote">Notice that since eSISE is not known for the user, the threshold T is taken as a pessimistic estimate of eSISE.</ref>.
| |
| * The probability of simultaneous not detected faulty satellites is negligible.
| |
| [[File:SISA and SISMA illustration concept.png|none|thumb|400px|alt=SISA and SISMA illustration concept|'''''Figure 1:''''' SISA and SISMA illustration concept]]
| |
|
| |
| ''Other remarks:'' As commented in previous sections, among the Galileo Global Component, the Regional and Local components of Galileo will support External Regional Integrity Services (ERIS) or Local Services by disseminating for selected Galileo satellites integrity data generated by independent regional or local service providers.
| |
|
| |
| ==Notes==
| |
| <references group="footnote"/>
| |
|
| |
| ==References==
| |
| * Hernandez Mendel, C., Catalan Catalan, C., Fernandez Vidou, M. and Sardon Perez, E., 2008. The Galileo Ground Segment Integrity Algorithms: Design and Performance. International Journal of Navigation and Observation 2008, pp. 1–16.
| |
| * Oehler, V., Luongo, F., Trautenberg, H., J.P., B., J., K. and T., R., 2005. The Galileo Integrity Concept and Performance. In: Proceedings of GNSS 2005 - The European Navigation Conference.
| |
|
| |
|
|
| |
|
| [[Category:Fundamentals]] | | [[Category:Fundamentals]] |
| [[Category:GALILEO]] | | [[Category:GALILEO]] |
