发明名称 Method and device for calculating an integrity risk in a satellite referencing system
摘要 <p>#CMT# #/CMT# The method involves determining Galileo parameters based on Galileo integrity concept by determining signal in space accuracy (SISA), signal in space monitoring accuracy (SISMA) and probability of ranging signal failures. The Galileo parameter is represented in a satellite based augmentation system (SBAS) parameter. Integrity risk for a satellite referencing system is determined based on a SBAS integrity concept under utilization of the SBAS parameter. #CMT# : #/CMT# Independent claims are also included for the following: (1) a computer program comprising instructions to perform a method for determining integrity risks in a satellite referencing system (2) a device for determining integrity risks in a satellite referencing system. #CMT#USE : #/CMT# Method for determining integrity risks in a satellite referencing system e.g. satellite navigation system. #CMT#ADVANTAGE : #/CMT# The method facilitates improved determination of the integrity risks in the satellite referencing system. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a flow diagram of a method for determining integrity risks in a satellite referencing system.'(Drawing includes non-English language text)'.</p>
申请公布号 EP2017636(B1) 申请公布日期 2013.06.19
申请号 EP20080012919 申请日期 2008.07.17
申请人 ASTRIUM GMBH 发明人 TRAUTENBERG, HANS L., DR.
分类号 G01S19/20;H04B17/40 主分类号 G01S19/20
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