Method and apparatus for integrity communication in a navigation satellite system

• US 8,072,375 B2
• Filed: 12/09/2009
• Issued: 12/06/2011
• Est. Priority Date: 12/10/2008
• Status: Expired due to Fees

• Current Assignee: Astrium GmbH (Airbus SE)
• Original Assignee: Astrium GmbH (Airbus SE)
• Inventors: Trautenberg, Hans L.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): Mull, Fred H
• Application Number:
  US12/634,295
• Publication Number:
  US 20100141512A1
• Time in Patent Office: 727 Days
• Field of Search: 342/357.395, 342/357.58
• US Class Current: 342/357.395
• CPC Class Codes: G01S 19/02 Details of the space or ground control segments
• CPC Class Codes: G01S 19/08 providing integrity information, e.g. health of satellites or quality of ephemeris data

Abstract

For integrity communication, a navigation satellite system has a space segment with satellites that emit navigation signals for reception and analysis by user systems, and a ground segment with observation stations that monitor the satellites. The ground segment controls cause distribution of integrity information concerning the satellites to user systems with the navigation signals. The integrity information has a first SISMA value and a second broadcast SISMA value for the accuracy of the satellite monitored by the ground segment. The second broadcast SISMA value takes into account a failure of an observation station of the ground segment, and a threshold value for the second broadcast SISMA value is provided. The threshold value with the integrity information for a satellite is transmitted 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. The integrity information to be transmitted when the second broadcast SISMA value and the first SISMA value for the satellite each exceed the threshold value.

Claims

1. 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.

2. The process according to claim 1, wherein the change of the integrity information comprises marking a particular satellite as “

not monitored”

in the integrity information.

3. The process according to claim 1, wherein the change of the integrity information comprises increasing the first SISMA value for a particular satellite with the integrity information.

4. A system 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 which monitor the satellites;

wherein;

the system is constructed for controlling the integrity communication such that it distributes integrity information concerning the satellites to user systems with the navigation signals;

the integrity information for a satellite has 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,

the second broadcast SISMA value, in contrast to the first SISMA value, takes into account a failure of an observation station of the ground segment;

a threshold value is provided for the second broadcast SISMA value; and

the system is configured to carry out the steps of,

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.