IP Library Granted Patent US 12,432,005
Granted Patent B2
US 12,432,005 · App. 18/181,459 · Granted Sep 30, 2025

Antenna steering through GNSS jamming, spoofing, and airplane maneuvers

Inventors: Vignesh Krishnan (Phoenix, AZ); Brian Schipper (Maple Grove, MN)
Assignee: Honeywell International Inc.
H04K3/224H04B7/043
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Quick Facts
Patent No.
US 12,432,005
App. No.
18/181,459
Granted
Sep 30, 2025
Kind
B2
Abstract

This disclosure describes systems and methods for providing antenna steering through GNSS jamming, spoofing, and airplane maneuvers. In certain embodiments, a device includes a GNSS antenna configured to receive GNSS signals transmitted from a plurality of GNSS sources; and a GNSS antenna support structure mounted within a vehicle, wherein the GNSS antenna is mounted to the GNSS antenna support structure, wherein the GNSS antenna support structure is configured to keep directionality of the GNSS antenna pointing up during motion of the vehicle.

Claims (35)

1. A device comprising:

a GNSS antenna configured to receive GNSS signals transmitted from a plurality of GNSS sources;

a GNSS antenna support structure mounted within a vehicle, wherein the GNSS antenna is mounted to the GNSS antenna support structure, wherein the GNSS antenna support structure is configured to keep directionality of the GNSS antenna pointing up during motion of the vehicle; and

a processor configured to:

calculate position adjustments to the GNSS antenna that keep the GNSS antenna pointing up during the motion of the vehicle; and

provide control signals to one or more actuators in the GNSS antenna support structure, wherein the control signals direct the one or more actuators to make the calculated position adjustments to the GNSS antenna.

2. The device of claim 1 , wherein the GNSS antenna support structure comprises a gimbal.

3. The device of claim 1 , wherein the GNSS antenna support structure comprises an actuator that moves the GNSS antenna in response to control signals.

4. The device of claim 3 , wherein the control signals are produced by a processor in response to navigation information acquired from one or more navigation sensors.

5. The device of claim 4 , wherein the processor is part of the GNSS antenna support structure.

6. The device of claim 1 , wherein the GNSS antenna support structure further keeps the directionality of the GNSS antenna pointing away from areas that pose a risk of containing one or more of interference signals and spoofing signals.

7. The device of claim 1 , wherein the GNSS antenna support structure maintains the GNSS antenna in a position that allows the GNSS antenna to continue receiving satellite signals through dynamic maneuvers.

8. The device of claim 1 , wherein the vehicle is an aircraft.

9. A method comprising:

receiving GNSS signals from a plurality of GNSS sources through a GNSS antenna, wherein the GNSS antenna is mounted on a GNSS antenna support structure that is mounted on a vehicle traveling over a terrain;

adjusting the GNSS antenna support structure to keep directionality of the GNSS antenna pointing in a direction away from earth that is perpendicular to a local horizontal plane;

calculating position adjustments to the GNSS antenna that keep the GNSS antenna pointing away from the terrain; and

providing control signals to one or more actuators in the GNSS antenna support structure, wherein the control signals direct the one or more actuators to make the calculated position adjustments to the GNSS antenna.

10. The method of claim 9 , wherein the GNSS antenna support structure comprises a gimbal.

11. The method of claim 10 , wherein the gimbal decouples GNSS antenna motion from the motion of the vehicle comprising pitch and roll.

12. The method of claim 9 , further comprising:

receiving navigational information representing the motion of the vehicle; and

moving the GNSS antenna to reflect the position adjustments.

13. The method of claim 9 , further comprising keeping the directionality of the GNSS antenna pointing away from areas that pose a risk of containing one or more of interference signals and spoofing signals.

14. The method of claim 9 , further comprising maintaining the GNSS antenna in a position that allows the GNSS antenna to continue receiving satellite signals through dynamic maneuvers.

15. The method of claim 9 , wherein the vehicle is an aircraft.

16. A system comprising:

a vehicle;

a GNSS antenna configured to receive GNSS signals transmitted from a plurality of GNSS sources; and

a GNSS antenna support structure mounted to a surface of the vehicle and to the GNSS antenna, wherein the GNSS antenna support structure is configured to decouple GNSS antenna motion from vehicle motion in at least pitch and roll; and

a processor configured to:

calculate position adjustments to the GNSS antenna that keep the GNSS antenna pointing away from terrain over which the vehicle travels; and

provide control signals to one or more actuators in the GNSS antenna support structure, wherein the control signals direct the one or more actuators to make the calculated position adjustments to the GNSS antenna.

17. The system of claim 16 , wherein the GNSS antenna support structure comprises a gimbal.

18. The system of claim 16 , wherein the GNSS antenna support structure further keeps the directionality of the GNSS antenna pointing away from areas that pose a risk of containing one or more of interference signals and spoofing signals.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 9, 2023
From: KRISHNAN, VIGNESH; SCHIPPER, BRIAN
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 062938/0610 →
Continuity (1)
Related Publication 20240305400A1 · Sep 12, 2024
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