{"id":238755,"date":"2024-10-19T15:36:17","date_gmt":"2024-10-19T15:36:17","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-en-61108-32010\/"},"modified":"2024-10-25T10:17:44","modified_gmt":"2024-10-25T10:17:44","slug":"bs-en-61108-32010","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-en-61108-32010\/","title":{"rendered":"BS EN 61108-3:2010"},"content":{"rendered":"
IEC 61108-3:2010 specifies the minimum performance standards, methods of testing and required test results for Galileo shipborne receiver equipment, based on IMO resolution MSC.233(82), which uses the signals from the Galileo Global Navigation Satellite System in order to determine position. It takes account of the general requirements given in IMO resolution A.694(17) and is associated with IEC 60945.<\/p>\n
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
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7<\/td>\n | CONTENTS <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | 1 Scope 2 Normative references <\/td>\n<\/tr>\n | ||||||
11<\/td>\n | 3 Terms, definitions and abbreviations 3.1 Terms and definitions 3.2 Abbreviations <\/td>\n<\/tr>\n | ||||||
12<\/td>\n | 4 Minimum performances standards 4.1 Object <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 4.2 Galileo receiver equipment 4.3 Performance standards for Galileo receiver equipment <\/td>\n<\/tr>\n | ||||||
16<\/td>\n | Tables Table 1 \u2013 Acquisition time limits <\/td>\n<\/tr>\n | ||||||
20<\/td>\n | Table 2 \u2013 RAIM integrity states <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | Table 3 \u2013 Integrity states corresponding to the Galileo integrity message <\/td>\n<\/tr>\n | ||||||
22<\/td>\n | 5 Methods of testing and required test results 5.1 Test sites Table 4 \u2013 Accuracy of COG <\/td>\n<\/tr>\n | ||||||
23<\/td>\n | 5.2 Test sequence 5.3 Test signals <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | 5.4 Determination of accuracy 5.5 General requirements and presentation requirements 5.6 Receiver tests <\/td>\n<\/tr>\n | ||||||
33<\/td>\n | 5.7 Tests for typical RF interference conditions <\/td>\n<\/tr>\n | ||||||
34<\/td>\n | Table 5 \u2013 RF interference values <\/td>\n<\/tr>\n | ||||||
36<\/td>\n | Annex A (informative) Galileo navigation signals characteristics Table A.1 \u2013 General characteristics of the Galileo navigation signals <\/td>\n<\/tr>\n | ||||||
37<\/td>\n | Table A.2 \u2013 General characteristics of Galileo observables <\/td>\n<\/tr>\n | ||||||
38<\/td>\n | Annex B (informative) The Galileo integrity concept <\/td>\n<\/tr>\n | ||||||
40<\/td>\n | Figures Figure B.1 \u2013 Graphical illustration of SISA and SISMA [GIC05] <\/td>\n<\/tr>\n | ||||||
41<\/td>\n | Table B.1 \u2013 Integrity flag values <\/td>\n<\/tr>\n | ||||||
44<\/td>\n | Annex C (informative) Receiver autonomous integrity monitoring (RAIM) <\/td>\n<\/tr>\n | ||||||
45<\/td>\n | Figure C.1 \u2013 Navigation alerts and FDE events <\/td>\n<\/tr>\n | ||||||
46<\/td>\n | Figure C.2 \u2013 RNP parameters <\/td>\n<\/tr>\n | ||||||
47<\/td>\n | Figure C.3 \u2013 Receiver autonomous integrity monitoring (RAIM) <\/td>\n<\/tr>\n | ||||||
48<\/td>\n | Figure C.4 \u2013 Position errors <\/td>\n<\/tr>\n | ||||||
49<\/td>\n | Figure C.5 \u2013 Decision threshold and minimum detectable bias for the (W)SSE statistic <\/td>\n<\/tr>\n | ||||||
50<\/td>\n | Figure C.6 \u2013 Maximum residual test statistic <\/td>\n<\/tr>\n | ||||||
51<\/td>\n | Figure C.7 \u2013 Geometry screening <\/td>\n<\/tr>\n | ||||||
52<\/td>\n | Table C.1 \u2013 Galileo satellite failure [GIC05] <\/td>\n<\/tr>\n | ||||||
53<\/td>\n | Table C.2 \u2013 RAIM-FDE parameters <\/td>\n<\/tr>\n | ||||||
54<\/td>\n | Annex D (normative) Galileo standard received signals and interference environment Table D.1 \u2013 Minimum and maximum receiver power levels on ground Table D.2 \u2013 Minimum and maximum levels at antenna port and receiver input <\/td>\n<\/tr>\n | ||||||
55<\/td>\n | Figure D.1 \u2013 E5 in-band and near-band maximum CW RFI levels Table D.3 \u2013 Table of main characteristics of Figure D.1 above <\/td>\n<\/tr>\n | ||||||
56<\/td>\n | Figure D.2 \u2013 E1 in-band and near-band maximum CW RFI levels Table D.4 \u2013 Table of main characteristics of Figure D.2 <\/td>\n<\/tr>\n | ||||||
57<\/td>\n | Figure D.3 \u2013 E5 Maximum in-band CW\/NBI RFI levels Figure D.4 \u2013 E1 Maximum in-band CW\/NBI RFI levels Table D.5 \u2013 E5 maximum in-band RFI levels versus bandwidth <\/td>\n<\/tr>\n | ||||||
58<\/td>\n | Table D.6 \u2013 E5 maximum in-band RFI levels versus bandwidth <\/td>\n<\/tr>\n | ||||||
59<\/td>\n | Annex E (informative) Galileo RAIM testing <\/td>\n<\/tr>\n | ||||||
60<\/td>\n | Table E.1 \u2013 Scenario overview <\/td>\n<\/tr>\n | ||||||
61<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Maritime navigation and radiocommunication equipment and systems. Global navigation satellite systems (GNSS) – Galileo receiver equipment. Performance requirements, methods of testing and required test results<\/b><\/p>\n |