Patent ID: 8072375

Claim:
A process for integrity communication in a navigation satellite system, having i) a space segment with a plurality of satellites that emit navigation signals for reception and analysis by user systems for the position determination, and ii) a ground segment with a plurality of observation stations that monitor the satellites, wherein the ground segment controls the integrity communication so that it distributes integrity information concerning the satellites to user systems with the navigation signals, the integrity information for a satellite having a first SISMA (signal-in-space monitoring accuracy) value and a second broadcast SISMA value for the accuracy of the satellite monitoring by the ground segment, with the second broadcast SISMA value, in contrast to the first SISMA value, taking into account a failure of an observation station of the ground segment, and a threshold value for the second broadcast SISMA value being provided; said process comprising: transmitting the threshold value with the integrity information for a satellite instead of the second broadcast SISMA value when the latter exceeds the threshold value and the first SISMA value is lower than the threshold value for the satellite; and changing the integrity information to be transmitted as soon as the second broadcast SISMA value and the first SISMA value for the satellite each exceed the threshold value.