IP Library Granted Patent US 9,689,989
Granted Patent B2
US 9,689,989 · App. 13/860,951 · Granted Jun 27, 2017

Detection of falsified signals in a satellite navigation system

Inventors: Hans Trautenberg (Cologne, DE); Johann Vilzmann (Rosenheim, DE)
Assignee: Astrium GmbH
G01S19/215
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Quick Facts
Patent No.
US 9,689,989
App. No.
13/860,951
Granted
Jun 27, 2017
Kind
B2
Abstract

A device for detection of falsified signals in a satellite navigation system includes at least two antennas having one or more receivers for receiving navigation signals, a phase difference measuring unit for determining phase differences of the received navigation signals for each antenna, and a detection unit for detecting falsified navigation signals among the received navigation signals on the basis of the phase differences determined.

Claims (26)

1. A device for detection of falsified signals in a satellite navigation system, comprising:

at least two antennas having one or more receivers for receiving navigation signals;

a phase difference measuring unit configured to determine respective phase differences of the received navigation signals for each of the at least two antennas; and

a detection unit configured to detect falsified navigation signals among the received navigation signals by comparing the determined phase differences,

wherein the detection unit is configured to determine that the navigation signals are falsified navigation signals when the phase differences of the navigation signals of the at least two antennas are approximately identical.

2. The device according to claim 1 , wherein the phase difference measuring unit is configured to determine the phase differences between the navigation signals received by the at least two antennas based on carrier phase measurements.

3. The device according to claim 2 , further comprising:

a reference wave unit configured to generate a reference wave with a same frequency as a carrier wave of the received navigation signals, the reference wave having a reference phase,

wherein the phase difference measuring unit is configured to determine the phase differences between the navigation signals received by the at least two antennas on the basis of measurements of the phase differences between the carrier phases of individual navigation signals and the reference phase.

4. The device according to claim 1 , wherein the at least two antennas are omnidirectional antennas.

5. A system that uses signals of a satellite navigation system, the system comprising:

a device comprising:

at least two antennas having one or more receivers for receiving navigation signals;

a phase difference measuring unit configured to determine respective phase differences of the received navigation signals for each of the at least two antennas; and

a detection unit configured to detect falsified navigation signals among the received navigation signals by comparing the determined phase differences; and

a navigation signal processing unit configured to process received navigation signals, such that navigation signals detected as falsified by the device are excluded from processing,

wherein the detection unit is configured to determine that the navigation signals are falsified navigation signals when the phase differences of the navigation signals of the at least two antennas are approximately identical.

6. A method for detecting falsified signals in a satellite navigation system, the method comprising:

receiving navigation signals via at least two antennas with one or more receivers;

determining, by a phase difference measuring unit, respective phase differences of the received navigation signals for each of the at least two antennas; and

determining, by a detection unit, that falsified navigation signals are among the received navigation signals by comparing the determined phase differences when the determined phase differences of the at least two antennas are approximately identical.

7. The method according to claim 6 , wherein the phase differences between the navigation signals received by the at least two antennas are determined by carrier phase measurements.

8. The method according to claim 7 , further comprising:

generating, by a reference wave unit, a reference wave at a same frequency as a carrier wave of the received navigation signals, the reference wave having a reference phase; and

determining the phase differences between the navigation signals received by the at least two antennas on the basis of measurements of the phase differences between the carrier phases of individual navigation signals and the reference phase.

9. The device according to claim 1 , wherein a difference of the phase differences of the navigation signals is compared to a predetermined threshold value.

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 Aug 11, 2016
From: TRAUTENBERG, HANS L.; VILZMANN, JOHANN
To: ASTRIUM GMBH
Reel/Frame 039409/0944 →
Priority Claims (1)
DE 10 2012 007 192 · Apr 12, 2012 · national
Continuity (1)
Related Publication 20130271316A1 · Oct 17, 2013