INMARSAT integrity channels for global navigation satellite systems

作者: G.V. Kinal , J. Nagle , D.W. Lipke

DOI: 10.1109/NTC.1992.267893

关键词:

摘要: It is pointed out that the transmission of integrity information using a signal format compatible with GPS (Global Positioning System) and relayed through geostationary satellite repeater will be critical in achieving high availability global navigation by satellite, along self-contained consistency checking techniques such as receiver autonomous monitoring. The next generation Inmarsat spacecraft, Inmarsat-3, contain repeaters designed to fulfill this function. system channel, use pseudorandom codes same family but distinct from reserved GPS. data basic channel convey user range error for 24 40 satellites. A closed-loop timing compensation technique used at uplinking earth station, make signal's clock carrier Doppler variations identical those would result an on-board source. Therefore, Inmarsat-3 satellites increase number useful available any user, can also function sources precise tuning. There possibility wide-area differential corrections carried on signal. >

参考文章(4)
J-M. DURAND, T. MICHAL, J. BOUCHARD, GPS Availability, Part I: Availability of Service Achievable for Different Categories of Civil Users Annual of Navigation. ,vol. 37, pp. 123- 139 ,(1990) , 10.1002/J.2161-4296.1990.TB01542.X
R. Braff, C.A. Shively, M.J. Zeltser, Radionavigation system integrity and reliability Proceedings of the IEEE. ,vol. 71, pp. 1214- 1223 ,(1983) , 10.1109/PROC.1983.12752
ALAN HOWELL, GEORGE KINAL, Inmarsat's third generation space segment 14th International Communication Satellite Systems Conference and Exhibit. ,(1992) , 10.2514/6.1992-1815
J. R. NAGLE, A. J. VAN DIERENDONCK, Q. D. HUA, INMARSAT-3 NAVIGATION SIGNAL C/A CODE SELECTION AND INTERFERENCE ANALYSIS Annual of Navigation. ,vol. 39, pp. 445- 461 ,(1992) , 10.1002/J.2161-4296.1992.TB02287.X