IP Library Granted Patent US 10,156,639
Granted Patent B2
US 10,156,639 · App. 13/524,227 · Granted Dec 18, 2018

Combined use of different satellite navigation systems

Inventor: Hans L. Trautenberg (Cologne, DE)
Assignee: ASTRIUM GMBH
G01S19/33G01S19/258G01S19/02G01S19/07G01S19/256
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Quick Facts
Patent No.
US 10,156,639
App. No.
13/524,227
Granted
Dec 18, 2018
Kind
B2
Abstract

Method, arrangement and system for improving a combined use of a plurality of different satellite navigation systems, in which each of the plurality of different satellite navigation systems includes a constellation of at least one satellite. The method includes broadcasting from each satellite of the constellation of a first satellite navigation system the clock models for all satellites of the constellation of a second satellite navigation system.

Claims (24)

1. An arrangement for improving a combined use of different satellite navigation systems, in which a first satellite navigation system includes a first constellation having at least one first satellite and a second satellite navigation system includes a second constellation having at least one second satellite, the arrangement comprising:

each at least one first satellite of the first constellation of the first satellite navigation system is structured and arranged to broadcast clock models for all second satellites of the second constellation of the second satellite navigation system, and

each at least one second satellite of the second constellation of the second satellite navigation system is structured and arranged to broadcast clock models for all first satellites of the first constellation of the first satellite navigation system,

whereby the at least one first and satellites of respective first and second satellite navigation systems are configured to transmit the clock models of the satellites of the respective other satellite navigation system.

2. The arrangement according to claim 1 , further comprising at least one first monitoring station of a first ground segment of the first satellite navigation system that is structured and arranged to monitor the broadcasting of clock models of the at least one first satellite.

3. The arrangement according to claim 2 , further comprising at least one second monitoring station of the second ground segment of the second satellite navigation system that is structured and arranged to monitor the broadcasting of the clock models of the at least one second satellite.

4. The arrangement according to claim 3 , further comprising a central unit structured and arranged to control the at least one first monitoring station and the at least one second monitoring station and to coordinate the broadcast of the clock models via the at least one first and second monitoring stations.

5. A receiver system for a combined use of a plurality of different satellite navigation systems, in which each of the plurality of different satellite navigation systems includes a constellation of at least one satellite, comprising:

a receiver structured and arranged to receive navigation signals from the at least one satellite of a first satellite navigation system and from the at least one satellite of a second navigation system, to receive clock models for all satellites of the second satellite navigation system broadcast from each at least one satellite of the first satellite navigation system, and to receive clock models for all satellites of the first satellite navigation system broadcast from each at least one satellite of the second satellite navigation system, whereby the satellites of the first and second satellite navigation systems are configured to transmit the clock models of satellites of the respective other satellite navigation system; and

a processor configured to consider the received clock models in evaluating navigation information contained in the received navigation signals of the satellites of the first and second satellite navigation systems.

6. The receiver system according to claim 5 , wherein the processor, in evaluating the navigation information, determines a current location of the receiver.

7. The receiver system according to claim 6 , further comprising a display structured and arranged to display the current location of the receiver.

8. The receiver system according to claim 5 , wherein the processor in evaluating the navigation signals considers orbit models of the first and second satellite navigation systems to be identical.

9. A system for use with a combined plurality of different satellite navigation systems, in which each of the plurality of different satellite navigation systems includes a constellation of at least one satellite, the system comprising:

a first ground segment monitoring station associated with a first satellite navigation system being structured and arranged to receive first clock models from the least one satellite of the first satellite navigation system;

a second ground segment monitoring station associated with a second satellite navigation system being structured and arranged to receive second clock models from the least one satellite of the second satellite navigation system; and

a control unit, which is coupled to the first and second ground segments, is configured to transmit the first clock signals to the second ground segment monitoring station, to transmit the second clock signals to the first ground segment monitoring station, to control the first ground segment monitoring station to actuate all of the satellites of the first satellite navigation system to broadcast the second clock signals with the navigation signals of the first satellite navigation system, and to actuate all of the satellites of the second satellite navigation system to broadcast the first clock signals with the navigation signals of the second satellite navigation system.

10. The system according to claim 9 , wherein the control unit is further structured and arranged to monitor the first ground segment monitoring station and the second ground segment monitoring station.

11. The system according to claim 10 , wherein the control unit is structured and arranged to monitor the first clock signals received by the first ground segment monitoring station.

12. The system according to claim 9 , wherein

the first ground segment monitoring station is further structured and arranged to transmit the second clock signals to the at least one satellite of the first satellite navigation system.

13. The system according to claim 12 , wherein the control unit is further structured and arranged to monitor the first ground segment monitoring station and the second ground segment monitoring station,

wherein, before transmitting the second clock signals to the first ground segment monitoring station, the control unit is structured and arranged to monitor the second clock signals received by the second ground segment monitoring station, and

wherein the control unit is structured and arranged to instruct the first ground segment monitoring station to transmit the second clock signals to the at least one satellite of the first navigation system.

Assignments (3)
MERGER Recorded Jan 10, 2019
From: AIRBUS DS GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 048043/0373 →
CHANGE OF NAME Recorded Oct 30, 2018
From: ASTRIUM GMBH
To: AIRBUS DS GMBH
Reel/Frame 047906/0600 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 20, 2012
From: TRAUTENBERG, HANS L., DR.
To: ASTRIUM GMBH
Reel/Frame 028993/0447 →
Priority Claims (1)
DE 10 2011 106 589 · Jun 16, 2011 · national
Continuity (1)
Related Publication 20130033398A1 · Feb 7, 2013