Compact single-aperture antenna and navigation system

• US 20080303714A1
• Filed: 05/29/2008
• Published: 12/11/2008
• Est. Priority Date: 05/29/2007
• Status: Abandoned Application

• Current Assignee: Toyon Research Corporation
• Original Assignee: Toyon Research Corporation
• Inventors: Werner, Benjamin D., Mujahed, Tariq A., Ezal, Kenan O.
• Application Number:
  US12/155,102
• Publication Number:
  US 20080303714A1
• Time in Patent Office: Days
• US Class Current: 342/357.12
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/45 by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
• CPC Class Codes: G01S 3/043 Receivers
• CPC Class Codes: G01S 3/32 derived from different combinations of signals from separate antennas, e.g. comparing sum with difference
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 1/38 formed by a conductive layer on an insulating support patch antennas H01Q9/0407; microstrip dipole antennas H01Q9/065; microstrip slot antennas H01Q13/106; transmission line microstrip antennas H01Q13/206; manufacturing reflecting surfaces using insulating material for supporting the reflecting surface H01Q15/142
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H01Q 9/27 Spiral antennas

Abstract

An exemplary radio-based navigation system uses a single-aperture multimode direction-finding antenna capable of determining platform position, velocity, attitude, and time while simultaneously providing protection against narrowband and broadband sources of interference. Global Navigation Satellite System (GNSS)-signals such as those from the Global Positioning System (GPS) provide protection against jammers while simultaneously providing attitude measurements with a compact single-aperture multimode antenna (e.g., a small two-arm spiral with improved angle-of-arrival performance over the entire hemisphere enhanced through the use of a conductive vertical extension of the antenna ground plane about the antenna perimeter and/or conductive posts placed evenly around the antenna perimeter). The multimode spiral may be treated as an array of cylindrically symmetric antenna elements. GPS receiver correlation architecture also may be modified for attitude determination by increasing the requisite number of input signals from one to at least two while minimizing the required number of correlators and mixers.

Claims

1. A single-aperture direction-finding antenna comprising:

a. a conductive ground surface;

b. a plurality of rotationally-symmetric conductive driven elements emanating from a common center above said conductive ground surface and supporting at least two direction-finding antenna modes while sharing a single radiating aperture; and

c. at least one rotationally-symmetric conductive member electrically connected to said conductive ground surface at a predetermined radius distance from said common center and extending away from the ground surface toward the driven elements while leaving a gap between said conductive driven elements and said conductive member,

whereby azimuthal phase and magnitude variations of said antenna modes are reduced resulting in improved angle-of-arrival accuracy and direction-finding performance over a hemisphere above said conductive ground surface.

2. The direction-finding antenna of claim 1 wherein said conductive driven elements comprise spiral arms.

3. The direction-finding antenna of claim 1 wherein said conductive member comprises a conductive wall located along an outer perimeter of said driven elements.

4. The direction-finding antenna of claim 1 wherein said conductive member comprises a set of conductive posts distributed about an outer perimeter of said driven elements.

5. The direction-finding antenna of claim 1 wherein

a. said conductive driven elements comprise spiral arms;

and

b. said conductive member comprises

(1) a cylindrical conductive wall located along a circular perimeter with a radius approximately equal to an outer radius of the spiral arms having a wall height less than the gap between the ground plane and the spiral arms; and

(2) a set of conductive posts distributed evenly about the circumference of said conductive wall wherein the posts are electrically connected to the wall and vertically extend to approximately the same height as the spiral arms.

6. A radio-based navigation system for receiving selected radio-frequency signals of a known origin and a known waveform, and for determining a the system position, velocity, attitude and time with simultaneous interference rejection, said system comprising.

a. at least one single-aperture direction-finding antenna with at least two feed ports and at least two direction-finding antenna modes;

b. a radio-frequency-to-digital receiver front-end connected to said at least two feed ports wherein said radio-frequency-to-digital receiver front-end at least down-converts each radio-frequency feed signal obtained from said at least two feed ports to respectively corresponding baseband signals; and

c. a digital electronics receiver module for at least computing the single-aperture antenna position, velocity, attitude, and time, and reducing the effects of interference, wherein said digital electronics receiver module;

(1) combines the baseband signals to form at least two antenna mode signals;

(2) combines the baseband signals or the antenna mode signals to create a primary navigation signal such that said selected radio-frequency signals are enhanced and/or the effects of external broadband interference signals, if any, are reduced;

(3) generates a replica waveform for each one of said select radio-frequency signals and produces a selected number of in-phase and quadrature-phase signals for said primary navigation signal and for each one of said antenna mode signals;

(4) determines the position, velocity, and time of the single-aperture antenna from at least the in-phase and the quadrature-phase signals corresponding to said primary navigation signal; and

(5) determines the attitude of the single-aperture antenna from at least the in-phase and the quadrature-phase signals corresponding to said antenna mode signals.

7. The radio-based navigation system of claim 6 wherein said single-aperture direction-finding antenna comprises a two-arm spiral antenna.

8. The radio-based navigation system of claim 6 wherein said select radio-frequency signals have been generated by at least one global navigation satellite system.

9. The radio-based navigation system of claim 6 wherein said select radio-frequency signals comprise global positioning system signals.

10. The radio-based navigation system of claim 7 wherein said radio-frequency-to-digital receiver further includes a common clock and common phased-lock loops for synchronously down-converting each of said radio-frequency feed signals.

11. The radio-based navigation system of claim 6 wherein said radio-frequency-to-digital receiver front-end further includes an analog mode-forming network.

12. The radio-based navigation system of claim 6 wherein said digital electronics receiver module reduces the effects of narrowband interference signals on the antenna mode signals and the primary navigation signal.

13. The radio-based navigation system of claim 6 wherein said digital electronics receiver module tracks phase modulation due to rotation, if any, of the single-aperture antenna about its boresight.

27. The radio-based navigation system of claim 6 wherein additional measurements from alternative sources are processed along with the in-phase and quadrature-phase signals to further improve the system position, velocity, attitude and time estimate.

29. The radio-based navigation system of claim 27 wherein the additional measurements are obtained from an inertial measurement unit.

31. The radio-based navigation system of claim 6 further comprising:

platform actuator and sensor measurement inputs;

a platform guidance and command system that generates platform commands using the system position, velocity, attitude and time estimates; and

a dynamic platform model that generates a platform state prediction based on the system position, velocity, attitude and time estimates, the platform commands, and the platform measurement inputs,

wherein the platform state prediction is fused with the in-phase and quadrature-phase signals to further improve the system position, velocity, attitude and time estimates.

33. The radio-based navigation system of claim 6 wherein the in-phase and quadrature-phase signals corresponding to the primary navigation signal and the antenna mode signals for said select radio-frequency signals are produced via a shared carrier- and code-tracking loop, thereby minimizing processing power requirements and system complexity.

14. A method for determining angle of arrival of received radio-frequency signals at a receiving single-aperture direction-finding antenna, said method comprising:

a. receiving radio-frequency signals via a plurality of rotationally-symmetric conductive driven elements emanating from a common center above a conductive ground surface, which elements support at least two direction-finding antenna modes while sharing a single radiating aperture;

b. providing at least one rotationally-symmetric conductive member electrically connected to said conductive ground surface at a predetermined distance from said common center and extending away from the ground surface toward the driven elements while leaving a gap between said conductive driven elements and said conductive member, and

c. determining angle-of-arrival of the received radio-frequency signals over a hemisphere above said conductive ground surface.

15. The method of claim 14 wherein said conductive driven elements comprise spiral arms.

16. The method of claim 14 wherein said conductive member comprises a conductive wall located along a circular perimeter of said driven elements with a radius approximately equal to an outer radius of said driven elements.

17. The method of claim 14 wherein said conductive member comprises a set of conductive posts distributed about a circular perimeter of said driven elements with a radius approximately equal to an outer radius of said driven elements.

18. The method of claim 14 wherein:

a. said conductive member comprises

(1) a cylindrical conductive wall located along a circular perimeter with a radius approximately equal to an outer radius of the spiral arms having a wall height less than the gap between the ground plane and the spiral arms; and

(2) a set of conductive posts distributed evenly about the circumference of said conductive wall wherein the posts are electrically connected to the wall and vertically extend to approximately the same height as the spiral arms.

19. A method for determining a radio signal receiver'"'"'s position, velocity, attitude and time with simultaneous interference rejection, said method comprising:

a. receiving selected radio-frequency signals of a known origin and waveform via at least one single-aperture direction-finding antenna with at least two feed ports and at least two direction-finding antenna modes;

b. connecting a radio-frequency-to-digital receiver front-end to said at least two feed ports wherein said radio-frequency-to-digital receiver front-end at least down-converts each radio-frequency feed signal obtained from said at least two feed ports to respectively corresponding baseband signals; and

c. computing the single-aperture antenna position, velocity, attitude, and time, and reducing the effects of interference, using a digital electronics receiver module which;

(1) combines the baseband signals to form at least two antenna mode signals;

(2) combines the baseband signals or the antenna mode signals to create a primary navigation signal such that said selected radio-frequency signals are enhanced and/or the effects of external broadband interference signals, if any, are reduced;

(3) generates a replica waveform for each one of said select radio-frequency signals and produces a selected number of in-phase and quadrature-phase signals for said primary navigation signal and for each one of said antenna mode signals;

(4) determines the position, velocity, and time of the single-aperture antenna from at least the in-phase and the quadrature-phase signals corresponding to said primary navigation signal; and

(5) determines the attitude of the single-aperture antenna from at least the in-phase and the quadrature-phase signals corresponding to said antenna mode signals.

20. The method of claim 19 wherein said single-aperture direction-finding antenna comprises a two-arm spiral antenna.

21. The method of claim 19 wherein said selected radio-frequency signals have been generated by at least one global navigation satellite system.

22. The method of claim 19 wherein said selected radio-frequency signals comprise global positioning system signals.

23. The method of claim 20 wherein said radio-frequency-to-digital receiver further includes a common clock and common phased-lock loops for synchronously down-converting each of said radio-frequency feed signals.

24. The method of claim 19 wherein said radio-frequency-to-digital receiver front-end further includes an analog mode-forming network.

25. The method of claim 19 wherein said digital electronics receiver module reduces the effects of narrowband interference signals on the antenna mode signals and the primary navigation signal.

26. The method of claim 19 wherein said digital electronics receiver module tracks phase modulation due to rotation, if any, of the single-aperture antenna about its boresight.

28. The method of claim 19 wherein additional measurements from alternative sources are fused with the in-phase and quadrature-phase signals to further improve the system position, velocity, attitude and time estimate.

30. The method of claim 19 wherein the additional measurements are obtained from an inertial measurement unit.

32. The method of claim 19 further comprising:

obtaining platform actuator and sensor measurement inputs;

generating platform commands using the system position, velocity, attitude and time estimates;

determining a platform state prediction based on a dynamic platform model, the system position, velocity, attitude and time estimates, the platform commands, and the platform measurement inputs; and

fusing the platform state prediction with the in-phase and quadrature-phase signals to further improve the system position, velocity, attitude and time estimates.

34. The method of claim 19 wherein the in-phase and quadrature-phase signals corresponding to the primary navigation signal and the antenna mode signals for said select radio-frequency signals are produced via a shared carrier- and code-tracking loop, thereby minimizing processing power requirements and system complexity.