WO2001031739A1 - Antenne microruban compacte pour applications gps - Google Patents

Antenne microruban compacte pour applications gps Download PDF

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Publication number
WO2001031739A1
WO2001031739A1 PCT/US2000/027855 US0027855W WO0131739A1 WO 2001031739 A1 WO2001031739 A1 WO 2001031739A1 US 0027855 W US0027855 W US 0027855W WO 0131739 A1 WO0131739 A1 WO 0131739A1
Authority
WO
WIPO (PCT)
Prior art keywords
edge
radiating element
ground plane
antenna
edges
Prior art date
Application number
PCT/US2000/027855
Other languages
English (en)
Inventor
Mohamed Sanad
Original Assignee
Antennas America, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Antennas America, Inc. filed Critical Antennas America, Inc.
Priority to AU34342/01A priority Critical patent/AU3434201A/en
Publication of WO2001031739A1 publication Critical patent/WO2001031739A1/fr

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • H01Q9/0421—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with a shorting wall or a shorting pin at one end of the element
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • H01Q9/0442—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular tuning means

Definitions

  • the present invention relates to antennas and more particularly to a compact microstrip antenna that is particularly suitable for Global Positioning System (GPS) applications.
  • GPS Global Positioning System
  • Prior known devices for GPS have generally been hand held or vehicle mounted.
  • the antennas for these GPS applications have generally been helix antennas or multilayer patch antennas . These antennas are complex and relatively expensive to manufacture.
  • GPS applications worn on the body such as for prisoner tracking
  • the body can interfere with the antenna function and the antenna must be capable of efficient function at any rotation in free space.
  • Antennas for such GPS systems must have good isotropic characteristics and be sensitive to circular polarization.
  • a compact microstrip antenna having a dielectric with a radiating element on a first side and a ground plane on a second side is disclosed.
  • the radiating element disclosed is substantially square with chamfered corners
  • the radiating element is partially shorted along a first edge to the ground plane through shorting posts extending through the dielectric.
  • the radiating element includes a reactance window parallel to and spaced from the first edge, and a feed point between the first edge and the reactance window.
  • Figure 1 is a perspective view of an antenna embodying features of the present invention.
  • Figure 2 is a top plan view of the antenna of Figure 1.
  • Figure 3 is a bottom plan view of the antenna of Figure 1.
  • the compact antenna embodying features of the present invention includes a dielectric 10, a radiating element 11, and a ground plane 12.
  • the dielectric 10 is generally a thin planar layer with a square outline, and includes a planar first side 14 and a spaced, oppositely facing planar second side 15.
  • the radiating element 11 is a substantially square thin layer of conductive material such as copper disposed on the first side 14 of the dielectric 10.
  • the radiating element 11 is slightly smaller than the first side 14 and a border 16 of first side 14 extends around the radiating element 11.
  • the radiating element 11 has a first edge 18, spaced second and third edges 19 and 20 extending transversely from opposite ends of the first edge 18, and a fourth edge 21, spaced from the first edge 18 and extending between the second and third edges 19 and 20.
  • the corners connecting the first, second, third and fourth edges 18, 19, 20 and 21 are chamfered so that the first, second, third and fourth edges 18, 19, 20 and 21 are connected by chamfer sections 22.
  • the chamfer sections 22 extend at 45 degrees relative to the first, second, third and fourth edges 18, 19, 20 and 21.
  • the chamfer sections 22 are preferably sized to reduce the length each of the first, second, third and fourth edges 18, 19, 20 and 21 by about 10% at each end, so that the length of the first and fourth edges 18 and 21 is about 80% of the distance from the second edge 19 to the third edge 20 and the length of the second and third edges 19 and 20 is about 80% of the distance from the first edge 18 to the fourth edge 21.
  • the ground plane 12 is truncated, having an area slightly larger than the area of the radiating element 11, and is disposed over substantially the entire second side 15 of the dielectric 10.
  • the antenna includes means for partially shorting the first edge 18 of the radiating element 11 to the ground plane 12.
  • the first edge 18 of the radiating element 11 is considered to be partially shorted because only a portion of the first edge 18 of is connected to the ground plane 12 instead of the entire first edge 18 of the radiating element 11.
  • the means for partially shorting includes a plurality of uniformly spaced shorting posts 24 in the form of plated through holes extending through the dielectric 10 and electrically connecting a portion of the first edge 18 to the ground plane 12.
  • the shorting posts 24 are linearly arranged along and as close as possible to the first edge 18 and are substantially centered along the first edge 18.
  • the means for partially shorting may alternatively include conductive tape or a tab extending around the dielectric 10 from the first edge 18 of the radiating element 11 to the ground plane 12.
  • the width of the means for partially shorting is preferably 35% to 55% of the distance from the second edge 19 to the third edge 20.
  • the radiating element 11 includes a feed point 27 located between the first edge 18 and the reactance window 25 and substantially centered between the second edge 19 and the third edge 20.
  • the feed point 27 includes a plated through hole through the dielectric 10.
  • the feed point 27 may alternatively include a non-plated hole.
  • the ground plane 12 includes an opening 28 around the feed point 27 on the second side 15 of the dielectric 10 so that the feed point 27 is electrically isolated from the ground plane 12.
  • a coaxial cable (not shown) in the embodiment shown may be attached to the antenna with the center conductor of the coaxial cable connecting to the feed point 27 at the second side 15 of the dielectric 10 and the outer conductor of the coaxial cable connecting to the ground plane 12.
  • an antenna as described above can be dimensioned as follows for GPS applications.
  • the dielectric 10 and the ground plane 12 each have a length of 24 mm and a width of 24 mm.
  • the dielectric is 3 mm thick.
  • the radiating element 11 is 22 mm wide and 22 mm long.
  • the corners of the radiating element are chamfered about 2 mm so that the first, second, third and fourth edges 18, 19, 20 and 21 are each 18 mm long and the chamfer sections 22 are about 2.8 mm.
  • the reactance window 25 is spaced 8 mm from the first edge 18, extends inward 11 mm from the second edge 19 and is 0.5 mm wide.
  • the feed point 27 is 1.4 mm in diameter, and is spaced 3 or 4 mm from the first edge 20.
  • the opening 28 in the ground plane 12, around the feed point 27 is 2.8 mm in diameter.
  • the antenna may be constructed of any other substrate material.
  • An exemplary material is MC3D Medium Frequency Laminate from GIL technologies, Collierville, Tennessee, with a dielectric constant of about 3.86.
  • the partial shorting of the radiating element 11 to the ground plane 12 reduces the size of the radiating element 11.
  • the reactance window 25 reduces the size of the radiating element 11 and increases the amount of diffracted waves, which improves the isotropic characteristics of the antenna and helps make the antenna sensitive to two perpendicular linear polarizations.
  • the square radiating element 11 and the chamfered sections 22 increase the sensitivity to circular polarization.
  • the truncation of the ground plane 12 reduces the antenna size and improves the isotropic characteristics.
  • the antenna of the present invention is significantly simpler and less expensive to manufacture than prior known antennas for GPS applications.

Landscapes

  • Waveguide Aerials (AREA)

Abstract

L'invention concerne une antenne microruban compacte pour applications GPS, comprenant un diélectrique (10) et un élément rayonnant carré (11) dont les coins (22) sont chanfreinés et le plan de sol tronqué (12). L'élément rayonnant (11) présente une fenêtre de réactance (25) servant à allonger le trajet du courant, ainsi qu'un point d'alimentation (27). Cet élément rayonnant (11) est partiellement mis en court-circuit avec le plan de sol (12). La fenêtre de réactance (25) et la mise en court-circuit partiel réduisent la taille de l'élément rayonnant (11). Cette antenne est compacte et présente de bonnes caractéristiques isotropes et une bonne sensibilité à la polarisation circulaire.
PCT/US2000/027855 1999-10-08 2000-10-06 Antenne microruban compacte pour applications gps WO2001031739A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU34342/01A AU3434201A (en) 1999-10-08 2000-10-06 Compact microstrip antenna for gps applications

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15850699P 1999-10-08 1999-10-08
US60/158,506 1999-10-08

Publications (1)

Publication Number Publication Date
WO2001031739A1 true WO2001031739A1 (fr) 2001-05-03

Family

ID=22568445

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2000/027855 WO2001031739A1 (fr) 1999-10-08 2000-10-06 Antenne microruban compacte pour applications gps

Country Status (2)

Country Link
AU (1) AU3434201A (fr)
WO (1) WO2001031739A1 (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1796212A1 (fr) * 2005-12-08 2007-06-13 Alps Electric Co., Ltd. Antenne à plaque
SG135069A1 (en) * 2006-02-24 2007-09-28 Sony Corp Compact omni-directional broadband monopole antenna
US7532164B1 (en) 2007-05-16 2009-05-12 Motorola, Inc. Circular polarized antenna
US8077092B2 (en) 2004-04-30 2011-12-13 Ecole Nationale Superieure Des Telecommunications De Bretagne Planar antenna with conductive studs extending from the ground plane and/or from at least one radiating element, and corresponding production method
US8738103B2 (en) 2006-07-18 2014-05-27 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US8896493B2 (en) 1999-10-26 2014-11-25 Fractus, S.A. Interlaced multiband antenna arrays
US8941541B2 (en) 1999-09-20 2015-01-27 Fractus, S.A. Multilevel antennae
US9331382B2 (en) 2000-01-19 2016-05-03 Fractus, S.A. Space-filling miniature antennas
US9755314B2 (en) 2001-10-16 2017-09-05 Fractus S.A. Loaded antenna
WO2018202495A1 (fr) 2017-05-02 2018-11-08 Atlas Elektronik Gmbh Corps sous-marin comprenant un élément hydrodynamique destiné à envoyer et/ou à recevoir un signal

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4040060A (en) * 1976-11-10 1977-08-02 The United States Of America As Represented By The Secretary Of The Navy Notch fed magnetic microstrip dipole antenna with shorting pins
US6140966A (en) * 1997-07-08 2000-10-31 Nokia Mobile Phones Limited Double resonance antenna structure for several frequency ranges
US6140968A (en) * 1998-10-05 2000-10-31 Murata Manufacturing Co., Ltd. Surface mount type circularly polarized wave antenna and communication apparatus using the same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4040060A (en) * 1976-11-10 1977-08-02 The United States Of America As Represented By The Secretary Of The Navy Notch fed magnetic microstrip dipole antenna with shorting pins
US6140966A (en) * 1997-07-08 2000-10-31 Nokia Mobile Phones Limited Double resonance antenna structure for several frequency ranges
US6140968A (en) * 1998-10-05 2000-10-31 Murata Manufacturing Co., Ltd. Surface mount type circularly polarized wave antenna and communication apparatus using the same

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8976069B2 (en) 1999-09-20 2015-03-10 Fractus, S.A. Multilevel antennae
US10056682B2 (en) 1999-09-20 2018-08-21 Fractus, S.A. Multilevel antennae
US9761934B2 (en) 1999-09-20 2017-09-12 Fractus, S.A. Multilevel antennae
US9362617B2 (en) 1999-09-20 2016-06-07 Fractus, S.A. Multilevel antennae
US9240632B2 (en) 1999-09-20 2016-01-19 Fractus, S.A. Multilevel antennae
US9054421B2 (en) 1999-09-20 2015-06-09 Fractus, S.A. Multilevel antennae
US9000985B2 (en) 1999-09-20 2015-04-07 Fractus, S.A. Multilevel antennae
US8941541B2 (en) 1999-09-20 2015-01-27 Fractus, S.A. Multilevel antennae
US8896493B2 (en) 1999-10-26 2014-11-25 Fractus, S.A. Interlaced multiband antenna arrays
US9905940B2 (en) 1999-10-26 2018-02-27 Fractus, S.A. Interlaced multiband antenna arrays
US10355346B2 (en) 2000-01-19 2019-07-16 Fractus, S.A. Space-filling miniature antennas
US9331382B2 (en) 2000-01-19 2016-05-03 Fractus, S.A. Space-filling miniature antennas
US9755314B2 (en) 2001-10-16 2017-09-05 Fractus S.A. Loaded antenna
US8077092B2 (en) 2004-04-30 2011-12-13 Ecole Nationale Superieure Des Telecommunications De Bretagne Planar antenna with conductive studs extending from the ground plane and/or from at least one radiating element, and corresponding production method
EP1796212A1 (fr) * 2005-12-08 2007-06-13 Alps Electric Co., Ltd. Antenne à plaque
SG135069A1 (en) * 2006-02-24 2007-09-28 Sony Corp Compact omni-directional broadband monopole antenna
US9899727B2 (en) 2006-07-18 2018-02-20 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US9099773B2 (en) 2006-07-18 2015-08-04 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US8738103B2 (en) 2006-07-18 2014-05-27 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US10644380B2 (en) 2006-07-18 2020-05-05 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US11031677B2 (en) 2006-07-18 2021-06-08 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US11349200B2 (en) 2006-07-18 2022-05-31 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US11735810B2 (en) 2006-07-18 2023-08-22 Fractus, S.A. Multiple-body-configuration multimedia and smartphone multifunction wireless devices
US7532164B1 (en) 2007-05-16 2009-05-12 Motorola, Inc. Circular polarized antenna
US7839339B2 (en) 2007-05-16 2010-11-23 Motorola Mobility, Inc. Circular polarized antenna
WO2018202495A1 (fr) 2017-05-02 2018-11-08 Atlas Elektronik Gmbh Corps sous-marin comprenant un élément hydrodynamique destiné à envoyer et/ou à recevoir un signal
DE102017109338A1 (de) * 2017-05-02 2018-11-08 Atlas Elektronik Gmbh Unterwasserkörper mit einem hydrodynamischen element zum senden und/oder empfangen eines signals

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Publication number Publication date
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