Multiband antenna

Abstract
A multi-band antenna comprising two or more low frequency radiators dimensioned to operate in a low frequency band, and two or more high frequency radiators dimensioned to operate in a high frequency band. Each high frequency radiator is substantially coplanar with the low frequency radiators, and is formed in a spiral with the high and low frequency radiators interleaved. A hybrid feed network has two or more antenna ports, each antenna port being coupled with a low frequency radiator and a high frequency radiator. The antenna can be used for receiving GPS L1/L2 signals. The antenna is configured to send and/or receive circularly polarized radiation.
Description




FIELD OF THE INVENTION




The invention relates to a multiband antenna, typically for receiving Global Positioning System (GPS) signals.




BACKGROUND OF THE INVENTION




Conventional two arm frequency independent Archimedean spiral antennas used to receive GPS L1/L2 signals exhibit poor group delay (d/df) variation performance over the hemispherical coverage required, and low efficiency. The variation rises from the movement of the active radiating region over the bandwidth of the GPS signal, multiple regions radiating beyond the primary region, and the use of only two ports. This variation degrades the performance of the system, requiring corrections in software to offset the variation. The variation is also undesirable in GPS surveying applications where low group delay variation is critical to obtain extremely accurate GPS locations. Low efficiency causes difficulty in acquiring low angle satellite signals and arises from the balun assembly needed to feed the two spiral ports, and current losses in the arms before reaching the radiating region.




WO 01/13465 (Kunysz) discloses an aperture coupled slot array antenna. Energy is coupled into each slotted opening by a transmission line in the shape of a circular arc. An impedance load is coupled to a terminal end of the transmission line to provide a leaky-wave antenna configuration and to thus ensure a uniform amplitude coupling to all slotted openings.




U.S. Pat. No. 3,949,407 (Jagdmann) discloses a spiral antenna in which the outer ends of the spiral arms are direct fed by a hybrid feed network. A multi-band antenna is disclosed with interleaved sets of low frequency and high frequency slotted openings.




U.S. Pat. No. 6,181,277 (Kesler) discloses a dual frequency microstrip patch antenna. A top microstrip patch element is separated from the ground plane by a larger second microstrip patch element. The top microstrip patch element is driven by a feed network consisting of three hybrid couplers.




U.S. Pat. No. 5,621,422 (Wang) discloses a two arm spiral-mode microstrip antenna in which the spiral arms are driven by a hybrid circuit with either 0 degree or 180 degree phase shift between the two arms.




U.S. Pat. No. 5,838,282 (Lalezari) discloses a multi-frequency antenna in which high frequency and low frequency radiating elements are each driven by respective feed circuits. A stacked patch antenna operates in a first frequency band and a crossed dipole element operates in a second frequency band.




U.S. Pat. No. 3,039,099 (Chait) discloses a linearly polarized spiral antenna system. Two spiral arms are coupled at both ends to a drive circuit.




U.S. Pat. No. 6,166,694 (Ying) discloses a printed twin spiral dual band antenna. A single (relatively long) low frequency spiral arm and a single (relatively small) high frequency spiral arm are coupled with a feeding pin, matching bridge, loading resistor and grounded post.




U.S. Pat. No. 3,925,784 (Phelan) discloses a 4-arm spiral antenna with inner ends coupled to a network of diodes, and outer ends coupled to switches.




U.S. Pat. No. 5,300,936 (Izadian) discloses a multiple band antenna, including one embodiment (FIG. 8) in which an array of four longitudinal radiating elements form two orthogonal dipole pairs. Hybrid circuits provide output signals in response to illumination of the dipole pairs.




U.S. Pat. No. 4,912,481 (Mace) discloses a multi-frequency antenna array in which an array of patches operable at high frequencies define a rectangular grid which is operable at low frequencies.




The paper E. Gschwendtner, W. Wiesebeck, “Low-Cost Spiral Antenna with Dual-Mode Radiation Pattern for Integrated Radio Services”, available at www.comcar.de/papers/ap2000.pdf describes a four arm spiral antenna with a coplanar waveguide transmission line connected to the centre of the spiral.




U.S. Pat. No. 5,541,617 (Connolly) discloses a quadrifilar helix antenna in which a 180 hybrid circuit drives the four radiating elements.




U.S. Pat. No. 5,955,997 (Ho) discloses a microstrip-fed cylindrical slot antenna. The antenna is driven by a non-isolating inline power splitter with an excess quarter-wavelength line in one output arm which generates the required 90 degrees phase differentials between the radiating slots.




U.S. Pat. No. 6,201,513 (Ow) discloses a two-arm spiral antenna driven by a two port balun assembly.




It is an object of the invention to provide an alternative antenna and feed network configuration with improved characteristics, or at least to provide a useful alternative.




BRIEF DESCRIPTION OF EXEMPLARY EMBODIMENT




A first aspect of the exemplary embodiment provides a multi-band antenna comprising two or more low frequency radiators dimensioned to operate in a low frequency band; two or more high frequency radiators dimensioned to operate in a high frequency band, each high frequency radiator being substantially coplanar with the low frequency radiators; and a hybrid feed network having two or more antenna ports, each antenna port being coupled with one or more of the radiators.




A second aspect of the exemplary embodiment provides a multi-band antenna comprising two or more low frequency radiators dimensioned to operate in a low frequency band; two or more high frequency radiators dimensioned to operate in a high frequency band; and a feed network having two or more antenna ports, wherein each antenna port is coupled with a low frequency radiator and a high frequency radiator.











BRIEF DESCRIPTION OF THE DRAWINGS




The accompanying drawings which are incorporated in and constitute part of the specification, illustrate embodiments of the invention and, together with the general description of the invention given above, and the detailed description of the embodiments given below, serve to explain the principles of the invention.





FIG. 1

is a perspective view of an antenna;





FIG. 2

is an exploded view of the antenna of

FIG. 1

;





FIG. 3

is a plan view of the antenna of

FIG. 1

;





FIG. 4

is a circuit diagram of the feed network; and





FIG. 5

is a circuit diagram of an alternative feed network.











DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION




Referring to

FIGS. 1-3

, the structure of the antenna


1


is formed by a cylindrical metal side wall


2


, metal disc


3


which forms the antenna ground plane, and a thin, low dielectric constant substrate


4


. The cylindrical cavity


5


formed by wall


2


and discs


3


,


4


is empty. The upper surface of disc


4


is initially coated in a continuous layer of metal, which is etched away to leave the pattern shown in

FIGS. 1-3

.




Referring to the plan view of

FIG. 3

, the pattern comprises a first set of four low-frequency arms


10


-


13


interleaved with a second set of four high-frequency arms


14


-


17


. The arms


10


-


13


are relatively long and are resonant at the lower L2 Global Positioning System (GPS) frequency of 1227.6 MHz. The arms


14


-


17


are relatively short and are resonant at the higher L1 GPS frequency of 1575.42 MHz. The ground plane disc


3


is spaced by a distance corresponding to approximately ½ or ¼ of the L1/L2 wavelengths.




The arms


10


-


17


are divided into four pairs, each pair branching out from a common respective power splitter junction (an exemplary junction being labelled


8


in FIG.


3


). The physical geometry of the antenna arms


10


-


17


will now be described with reference to exemplary arms


14


and


13


. Arm


14


has a radially extending straight portion


25


and a straight portion


26


extending tangentially from the power splitter junction


8


. Arm


13


has a radially extending straight portion


27


and a straight portion


28


extending tangentially from the power splitter junction. The arms are formed in a spiral, with the curved portions of the longer low frequency arms


10


-


13


subtending an angle of approximately 230 degrees, and the curved portions of the shorter low frequency arms


14


-


17


subtending an angle of approximately 170 degrees.




The power splitter input lines


18


are each soldered to a respective antenna port of a feed network


19


. One of the antenna ports is labelled at


20


in FIG.


1


.




Referring to

FIG. 4

, the feed network


19


is a monolithic Anaren Xinger™ delay line chip, model no. 21B1305 having a −90 degree port


30


, 0 degree port


31


, −180 degree port


32


, −270 degree port


33


, and input port


34


. An incoming signal on input port


34


is divided into two equal signals, offset by 180 degrees, by a directional coupler


35


on 0 degree line


36


and −180 degree line


37


. The 0 degree signal is input to a 3 dB 90 degree coupled line hybrid


38


and the −180 degree signal is input to a 3 dB 90 degree coupled line hybrid


39


. The 90 degree and −90 degree output lines of hybrids


38


,


39


form the four antenna ports


30


-


33


. The fourth ports


40


,


41


of hybrids


38


,


39


are terminated. Thus a signal input to input port


34


is divided into four equal amplitude signals each having a quadrature phase offset, thus resulting in a circularly polarized radiation beam.




Input/output signals are transmitted to/from the port


34


by via an SMA connector


40


and transmission line


41


(FIG.


2


). The connector


40


is coupled to a receiver or low noise amplifier (not shown).




An alternative feed network


50


is shown in FIG.


5


. The network is identical to the network


19


of

FIG. 4

, except that the directional coupler


35


is replaced by a 3 dB 90 degree coupled line hybrid


51


with a Schiffman phase shifter


52


to alter the −90 degree leg


53


by a further 90 degrees.




Both feed networks


19


and


50


are fabricated using stripline techniques. This is relatively expensive (compared with microstrip techniques) but much broader frequency response is the payoff.




The use of hybrid feed networks


51


,


35


results in improved efficiency and simpler production compared with the two port balun assembly described in U.S. Pat. No. 6,201,513 (Ow). The feed networks provide a direct path to the resonant arms, minimising current losses. Radiation pattern performance is well suited to satellite communications.




By coupling a low frequency arm and a high frequency arm with each antenna port via a power splitter, the antenna only requires a single four port hybrid feed network to drive all eight arms.




The antenna has extremely low group delay variation due to the four arm structure, and lack of multiple radiation regions.




While the present invention has been illustrated by the description of the embodiments thereof, and while the embodiments have been described in detail, it is not the intention of the Applicant to restrict or in any way limit the scope of the appended claims to such detail. Additional advantages and modifications will readily appear to those skilled in the art. Therefore, the invention in its broader aspects is not limited to the specific details, representative apparatus and method, and illustrative examples shown and described. Accordingly, departures may be made from such details without departure from the spirit or scope of the Applicant's general inventive concept.




For instance, the arms


10


-


17


may be replaced by slotted openings as described in WO 01/13465 (Kunysz). Frequency of operation and impedance can be altered by adjusting the arm length and pitch angle.




Although the preferred embodiment is operated in receive mode for receiving satellite GPS signals, the antenna could also be operated in transmit mode for other applications. The antenna could also be operated in both transmit and receive mode, either simultaneously or alternately. Thus it will be understood that the term “radiating element” in the appended claims refers to an element which can transmit and/or receive electromagnetic energy.




The invention may be utilised with other radiator constructions: for instance an array of dipoles or patch elements, or a quadrifilar helix.



Claims
  • 1. A multi-band antenna comprising two or more low frequency radiators dimensioned to operate in a relatively low frequency band; two or more high frequency radiators dimensioned to operate in a relatively high frequency band, each high frequency radiator being substantially coplanar with the low frequency radiators; and a hybrid feed network having two or more antenna ports, each antenna port being coupled with one or more of the low frequency and high frequency radiators and where the low frequency and high frequency radiators coupled to the ports further comprise at least one low frequency radiator and at least one high frequency radiator.
  • 2. An antenna according to claim 1, wherein the low and high frequency radiators are spiral arms, with the low frequency spiral arms being interleaved with the high frequency spiral arms.
  • 3. An antenna according to claim 2 wherein the spiral arms have curved portions which subtend an angle less than 360 degrees.
  • 4. An antenna according to claim 2 wherein the low and/or high frequency arms include a tangentially extending straight portion.
  • 5. An antenna according to claim 1 wherein the radiators comprise conducting arms.
  • 6. An antenna according to claim 1 wherein each antenna port of the feed network is at a different phase.
  • 7. An antenna according to claim 1 wherein the antenna is configured to send and/or receive circularly polarized radiation.
  • 8. An antenna according to claim 1 wherein the feed network has four or more antenna ports.
  • 9. An antenna according to claim 1 comprising four or more low frequency radiators, and four or more high frequency radiators.
  • 10. An antenna according to claim 9 consisting of four low frequency radiators, and four high frequency radiators.
  • 11. An antenna according to claim 1 wherein the low and high frequency radiators are elongated along respective lengths, and wherein the length of the low frequency radiators is greater than the length of the high frequency radiators.
  • 12. An antenna according to claim 1 wherein the radiators extend outwardly from a common central region.
  • 13. An antenna according to claim 12 wherein the radiators have inner ends proximate to the central region which are coupled to the feed network.
  • 14. An antenna according to claim 1 configured to receive GPS signals.
  • 15. An antenna according to claim 1 wherein the feed network comprises a first power divider having an input port and first and second output lines which are phase offset, second and third power dividers each having an input line and first and second output ports which are phase offset, wherein the input line of the second power divider is coupled to the first output line of the first power divider, and the input line of the third power divider is coupled to the second output line of the first power divider.
  • 16. An antenna according to claim 15 wherein the second and third power dividers comprise hybrid circuits.
  • 17. An antenna according to claim 16 wherein the hybrid circuits are coupled line hybrid circuits.
  • 18. An antenna according to claim 1 wherein the feed network includes one or more coupled line hybrid circuits.
  • 19. An antenna according to claim 15 wherein the first power divider comprises a directional coupler.
  • 20. An antenna according to claim 15 wherein the first power divider comprises a hybrid circuit.
  • 21. An antenna according to claim 1 wherein the radiators are microstrip or stripline radiators.
  • 22. An antenna according to claim 1 including a ground plane spaced from the radiators by a distance which is less than the resonant wavelength of the high frequency radiators.
  • 23. An antenna according to claim 1 wherein the radiators are positioned adjacent to a cavity defined by a ground plane and conductive side walls.
  • 24. A multi-band antenna comprising two or more low frequency radiators dimensioned to operate in a relatively low frequency band; two or more high frequency radiators dimensioned to operate in a relatively high frequency band; and a feed network having two or more antenna ports, wherein each antenna port is coupled with a low frequency radiator and a high frequency radiator.
  • 25. An antenna according to claim 24, wherein the low and high frequency radiators are spiral arms, with the low frequency spiral arms being interleaved with the high frequency spiral arms.
  • 26. An antenna according to claim 25 wherein the spiral arms have curved portions which subtend an angle less than 360 degrees.
  • 27. An antenna according to claim 25 wherein the low and/or high frequency arms include a tangentially extending straight portion.
  • 28. An antenna according to claim 24 wherein the radiators comprise conducting arms.
  • 29. An antenna according to claim 24 wherein each antenna port of the feed network is at a different phase.
  • 30. An antenna according to claim 24 wherein the antenna is configured to send and/or receive circularly polarized radiation.
  • 31. An antenna according to claim 24 wherein the feed network has four or more antenna ports.
  • 32. An antenna according to claim 24 comprising four or more low frequency arms, and four or more high frequency arms.
  • 33. An antenna according to claim 32 consisting of four low frequency arms, and four high frequency arms.
  • 34. An antenna according to claim 24 wherein the low and high frequency radiators are elongated along respective lengths, and wherein the length of the low frequency radiators is greater than the length of the high frequency radiators.
  • 35. An antenna according to claim 24 wherein the radiators extend outwardly from a common central region.
  • 36. An antenna according to claim 24 wherein the radiators have inner ends proximate to the central region which are coupled to the feed network.
  • 37. An antenna according to claim 24 configured to received GPS signals.
  • 38. An antenna according to claim 24 wherein the feed network comprises a first power divider having an input port and first and second output lines which are phase offset, second and third power dividers each having an input line and first and second output ports which are phase offset, wherein the input line of the second power divider is coupled to the first output line of the first power divider, and the input line of the third power divider is coupled to the second output line of the first power divider.
  • 39. An antenna according to claim 38 wherein the second and third power dividers comprise hybrid circuits.
  • 40. An antenna according to claim 39 wherein the hybrid circuits are coupled line hybrid circuits.
  • 41. An antenna according to claim 24 wherein the feed network includes one or more coupled line hybrid circuits.
  • 42. An antenna according to claim 38 wherein the first power divider comprises a directional coupler.
  • 43. An antenna according to claim 38 wherein the first power divider comprises a hybrid circuit.
  • 44. An antenna according to claim 24 wherein the radiators are microstrip or stripline radiators.
  • 45. An antenna according to claim 24 including a ground plane spaced from the radiators by a distance which is less than the resonant wavelength of the high frequency radiators.
  • 46. An antenna according to claim 24 wherein the radiators are positioned adjacent to a cavity defined by a ground plane and conductive side walls.
US Referenced Citations (18)
Number Name Date Kind
3039099 Chait et al. Jun 1962 A
3828351 Voronoff Aug 1974 A
3925784 Phelan Dec 1975 A
3949407 Jadgmann et al. Apr 1976 A
4912481 Mace et al. Mar 1990 A
5087922 Tang et al. Feb 1992 A
5300936 Izadian Apr 1994 A
5451973 Walter et al. Sep 1995 A
5541617 Connolly et al. Jul 1996 A
5621422 Wang Apr 1997 A
5838282 Lalezari et al. Nov 1998 A
5955997 Ho et al. Sep 1999 A
6166694 Ying Dec 2000 A
6181277 Kesler et al. Jan 2001 B1
6201513 Ow et al. Mar 2001 B1
6208312 Gould Mar 2001 B1
6252559 Donn Jun 2001 B1
6323820 Haunberger Nov 2001 B1
Foreign Referenced Citations (2)
Number Date Country
2000269736 Sep 2000 JP
WO 0113465 Feb 2001 WO
Non-Patent Literature Citations (1)
Entry
Paper of E. Gschwendtner and W. Wiesebeck, “Low-Cost Spiral Antenna with Dual-Mode Radiation Pattern for Integrated Radio Services”, available at www.comcar.de/papers/ap2000.pdf.