Spatial null steering microstrip antenna array

• US 6,597,316 B2
• Filed: 09/17/2001
• Issued: 07/22/2003
• Est. Priority Date: 09/17/2001
• Status: Active Grant

• Current Assignee: Mitre Corporation
• Original Assignee: Mitre Corporation
• Inventors: Rao, Barsur Rama, Rosario, Edward N.
• Primary Examiner(s): LE, HOANGANH T
• Application Number:
  US09/954,527
• Publication Number:
  US 20030052825A1
• Time in Patent Office: 673 Days
• Field of Search: H01/Q.138, 343/700.MS, 343/853, 343/850, 343/846, 343/848
• US Class Current: 343/700.0MS
• CPC Class Codes: H01Q 3/2629 Combination of a main antenna unit with an auxiliary antenna unit
• CPC Class Codes: H01Q 9/0407 Substantially flat resonant element parallel to ground plane, e.g. patch antenna dipole H01Q9/285; monopole H01Q9/40
• CPC Class Codes: H01Q 9/0435 using two feed points
• CPC Class Codes: H01Q 9/0464 Annular ring patch

Abstract

A spatial null steering microstrip antenna array comprising two concentric microstrip patch antenna elements. An inner circular antenna is used as an auxiliary element in nulling interference received by an outer annular ring antenna disposed around the inner antenna. The outer annular antenna is resonant in a higher order mode but forced to generate a right hand circularly polarized lower order (TM₁₁) far field radiation pattern, thereby allowing co-modal phase tracking between the two antenna elements for adaptive cancellation. Each antenna element is appropriately excited by symmetrically spaced probes. Other applications of the antenna array include GPS multipath suppression, simultaneous satellite and terrestrial communications, and co-site interference suppression. Dual frequency band applications are achieved by stacked array configurations.

Claims

1. A spatial null steering microstrip antenna array comprising:

an inner microstrip patch antenna for use as an auxiliary element in nulling interference;

an outer microstrip patch antenna disposed around the inner microstrip patch antenna, the outer microstrip patch antenna having a geometry symmetrical to the inner microstrip patch antenna and resonance in a higher-order mode;

a dielectric substrate layer below the inner microstrip patch antenna and outer microstrip patch antenna;

a conducting ground plane below the dielectric substrate layer extending beyond the outermost dimensions of the outer microstrip patch antenna;

a first set of four coaxial probes, each probe extending up through the conducting ground plane and the dielectric substrate layer and connected on one end to one of four points on the inner microstrip patch antenna symmetrically spaced at 90°

intervals;

a second set of four coaxial probes, each probe extending up through the conducting ground plane and the dielectric substrate layer and connected on one end to one of four points on the outer microstrip patch antenna symmetrically spaced at 90°

intervals;

wherein each of the first set and second set of probes are driven in equal amplitudes but at relative phase angles of 0°

, 90°

, 180°

, and 270°

respectively, thereby forcing the outer microstrip patch antenna and inner microstrip patch antenna to each generate a right hand circularly polarized lower order TM₁₁ mode far field radiation pattern and allowing co-modal phase tracking between the inner microstrip patch antenna and outer microstrip patch antennas; and

means for shaping a combined radiation pattern of the inner microstrip patch antenna and outer microstrip patch antennas to null out received signals from interference sources at a pre-selected elevation angle.

3. The spatial null steering microstrip antenna array of claims 1 or 2, wherein the conducting ground plane further comprises a resistivity tapered conducting ground plane for suppression of antenna back-lobes.

4. The spatial null steering microstrip antenna array of claims 1 or 2, wherein the conducting ground plane further comprises a film with a sputtered, tapered resistive film of Indium Tin Oxide, bonded to a thin plastic plate.

2. A spatial null steering microstrip antenna array comprising:

a circular microstrip patch antenna for use as an auxiliary element in nulling interference;

an annular ring microstrip patch antenna disposed around the circular microstrip patch antenna, the annular ring microstrip patch antenna having a geometry symmetrical to the circular microstrip patch antenna and resonance in a higher-order TM₄₁ mode;

a dielectric substrate layer below the circular microstrip patch antenna and annular ring microstrip patch antenna;

a conducting ground plane below the dielectric substrate layer extending beyond the outer diameter of the annular ring microstrip patch antenna;

a first set of four coaxial probes, each probe extending up through the conducting ground plane and the dielectric substrate layer and connected on one end to one of four points on the circular microstrip patch antenna symmetrically spaced at 90°

intervals;

a second set of four coaxial probes, each probe extending up through the conducting ground plane and the dielectric substrate layer and connected on one end to one of four points on the outer microstrip patch antenna symmetrically spaced at 90°

intervals;

wherein each of the first set and second set of probes are driven in equal amplitudes but at relative phase angles of 0°

, 90°

, 180°

, and 270°

respectively, thereby forcing the outer microstrip patch antenna and circular microstrip patch antenna to each generate a right hand circularly polarized lower order TM₁₁ mode far field radiation pattern and allowing co-modal phase tracking between the circular microstrip patch antenna and outer microstrip patch antennas; and

means for shaping a combined radiation pattern of the circular microstrip patch antenna and annular ring microstrip patch antennas to adaptively cancel received interference signals at a pre-selected elevation angle.

5. A GPS multipath suppression antenna array, comprising

an annular ring antenna for receiving GPS signals resonant in a higher order TM₄₁ mode;

a circular mnicrostrip antenna concentrically positioned within the annular ring antenna for use as an auxiliary element in cancelling out cross polarized LHCP multipath signals received by the annular ring antenna;

a dielectric substrate layer sandwiched below the antennas and above a resistivity tapered ground plane; and

a means for exciting both the circular microstrip antenna and the annular ring antenna to generate RHCP lower order TM₁₁ mode far field radiation patterns, allowing the annular ring radiation pattern to phase track the radiated signals from the circular microstrip antenna to allow cancellation of the cross polarized GPS multipath at a desired elevation angle.

6. A dual frequency GPS multipath suppression antenna array, comprising:

a first annular ring antenna for receiving GPS signals in a first frequency band resonant in a higher order TM₄₁ mode;

a first circular microstrip antenna concentrically positioned within the first annular ring antenna for use as an auxiliary element in cancelling out cross polarized LHCP multipath signals received by the first annular ring antenna;

a first dielectric substrate layer sandwiched beneath the first antennas and above a resistivity tapered ground plane;

a second dielectric substrate layer stacked on top of the first circular and first annular ring antennas,

a second annular ring antenna for receiving GPS signals in a second frequency band resonant in a higher order TM₁₁ mode stacked on top of the second dielectric substrate layer and positioned coaxially above the first annular ring antenna;

a second circular microstrip antenna positioned within the second annular ring antenna and stacked on top of the second dielectric substrate layer and positioned coaxially above the first circular microstrip antenna;

means for exciting both the first circular microstrip antenna and the first annular ring antenna to generate RHCP lower order TM₁₁ mode far field radiation patterns, allowing the first annular ring radiation pattern to phase track the radiated signals from the first circular microstrip antenna to allow cancellation of the cross polarized GPS multipath at a desired elevation; and

means for exciting both the second circular microstrip antenna and the second annular ring antenna to generate RHCP lower order TM₁₁ mode far field radiation patterns, allowing the second annular ring radiation pattern to phase track the radiated signals from the second circular microstrip antenna to allow cancellation of the cross polarized GPS multipath at a desired elevation angle.

7. An dual use satellite and terrestrial communications antenna array, comprising:

a circular microstrip patch antenna generating a single lobe, circularly polarized antenna pattern directed towards zenith for communicating with the satellite at a desired SATCOM frequency;

an annular ring microstrip patch antenna disposed around the circular microstrip patch antenna, the annular ring mnicrostrip patch antenna being resonant in a higher order TM₄₁ mode, but simultaneously generating a zero order (TEM type), doughnut shaped, modal pattern with peak gain at horizon and a null at zenith for communicating terrestrially at a desired frequency;

a dielectric substrate layer sandwiched beneath the circular microstrip patch antenna and annular ring microstrip patch antenna and above a conducting ground plane;

a plurality of coaxial probes, each probe extending through the conducting ground plane and dielectric substrate layer, for exciting the circular microstrip patch antenna or the annular ring microstrip patch antenna.

8. The antenna array of claim 7, wherein the conducting ground plane is metallic.

9. The antenna array of claim 7, wherein the conducting ground plane is a resistivity tapered conducting ground plane.

10. The antenna array of claim 7, wherein the circular microstrip patch antenna and annular ring microstrip patch antenna are each tuned to a separate frequency to allow simultaneous communications with both the SATCOM and terrestrial communications systems.