COMPACT SINGLE-APERTURE ANTENNA AND DIRECTION-FINDING NAVIGATION SYSTEM

• US 20110304507A1
• Filed: 08/12/2011
• Published: 12/15/2011
• Est. Priority Date: 05/29/2007
• Status: Active Grant

• Current Assignee: Toyon Research Corporation
• Original Assignee: Toyon Research Corporation
• Inventors: Mujahed, Tariq A., Ezal, Kenan O.
• Granted Patent: US 8,704,728 B2
• Time in Patent Office: Days
• US Class Current: 342/417
• 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

A radio-based navigation system uses a small multi-mode direction-finding antenna and a direction-finding receiver to determine 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 a Global Positioning System (GPS) provide attitude measurements with a compact multi-mode direction-finding antenna (e.g., a small two-arm spiral with improved angle-of-arrival performance over the entire hemisphere enhanced through 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) that provides protection against jammers. The multi-mode spiral may be treated as an array of rotationally-symmetric antenna elements. The GPS receiver architecture may be modified for direction-finding and thereby attitude determination by increasing the 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. at least one conductive driven element located above a conductive ground surface;

b. a plurality of feed ports driving said at least one conductive driven element, wherein the feed ports and the driven element are rotationally-symmetric about a common center above said conductive ground surface and support 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 distance from said common center and extending away from the ground surface toward said at least one conductive driven element while leaving a gap between said at least one conductive driven element 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 at least one conductive driven element comprises 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 at least one conductive driven element.

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 at least one conductive driven element.

5. The direction-finding antenna of claim 1, wherein:

a. said at least one conductive driven element comprises 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 surface 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 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 feed ports for at least one rotationally-symmetric conductive driven element emanating from a common center above a conductive ground surface, wherein said at least one conductive driven element and the feed ports 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 said at least one conductive driven element while leaving a gap between said at least one conductive driven element and said conductive member; and

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

7. The method of claim 6, wherein said at least one conductive driven element comprises spiral arms.

8. The method of claim 6, wherein said conductive member comprises a conductive wall located along an outer perimeter of said at least one conductive driven element.

9. The method of claim 6, wherein said conductive member comprises a set of conductive posts distributed about an outer perimeter of said at least one conductive driven element.

10. The method of claim 6, wherein:

a. said at least one rotationally-symmetric conductive driven element comprises 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.