Two-Sided Overlapping Coupled Sectorial Loop Antenna

Abstract

A two-sided overlapping coupled sectorial loop antenna (CSLA). The CSLA includes a ground plane and a dielectric substrate mounted substantially perpendicular thereto. A first metalized trace is deposited on one side of the substrate and a second metalized trace is deposited on the other side of the substrate, where the metalized traces overlap at a center area and are coupled to a common feed at the center area. In one embodiment, the size of the CSLA is further reduced by adding inductors to the traces.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates generally to a compact and wide-band coupled sectorial loop antenna (CSLA) and, more particularly, to a two-sided coupled sectorial loop antenna having a sectorial loop deposited on opposing sides of a dielectric substrate.

2. Discussion of the Related Art

Various applications for ultra-wideband (UWB) wireless systems are known in the art, including ground penetrating radar, high data rate short range wireless local area networks, communication systems for military applications, UWB short pulse radars for automotive and robotics applications, etc. UWB wireless systems require antennas that are able to operate across a very large bandwidth with consistent polarization and radiation pattern parameters over the entire band. Various techniques are known in the art to design antennas with wideband impedance matched characteristics.

Traveling wave antennas and antennas with topologies that are invariant by rotation are inherently wideband and have been extensively used in the art. Self-complimentary antenna concept provides a constant input impedance irrespective of frequency, provided that the size of the ground plane for the slot segment of the antenna is large and an appropriate self-complimentary feed can be designed. Theoretically, the input impedance of self-complimentary antennas is 186 ohms, and thus, these antennas cannot be directly matched to standard transmission lines having a 50 ohm impedance. Another drawback of self-complimentary antenna structures is that they cannot be printed on a dielectric substrate because the dielectric constant of the substrate perturbs the self-complimentary condition.

Another technique for designing wideband antennas is to use multi-resonant radiation structures. Log-periodic antennas, microstrip patches with parasitic elements, and slotted microstrip antennas for broadband and dual-band applications are examples of such multi-resonant radiating structures.

The electric dipole and monopole above a ground plane are perhaps the most basic types of antennas. Variations of these antennas have recently been introduced for obtaining considerably larger bandwidths than the traditional dipole and monopole antenna designs. Impedance bandwidth characteristics of circular and elliptical monopole plate antennas are also known in the art. Wideband characteristics of rectangular and square monopole antennas are also known, and a dielectric loaded wideband monopole has been investigated in the art. One drawback of these types of antennas is that the antenna polarization as a function of frequency changes.

SUMMARY OF THE INVENTION

In accordance with the teachings of the present invention, a two-sided overlapping coupled sectorial loop antenna (CSLA) is disclosed. The CSLA includes a ground plane and a dielectric substrate mounted substantially perpendicular thereto. A first metalized trace is deposited on one side of the substrate and a second metalized trace is deposited on the other side of the substrate, where the metalized traces overlap at a center area and are coupled to a common feed at the center area. In one embodiment, the size of the CSLA is further reduced by adding inductors to the traces.

Additional features of the present invention will become apparent from the following description and appended claims, taken in conjunction with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a plan view of a sectorial loop antenna, according to an embodiment of the present invention;

FIG. 2 is a plan view of two parallel sectorial loop antennas that are proximity coupled to each other;

FIG. 3 is a plan view of a coupled sectorial loop antenna, according to an embodiment of the present invention;

FIGS. 4(a)-4(j) are graphs with C/λ on the horizontal axis, where C=2πR_out, and impedance on the vertical axis showing self and mutual impedances of the SLAs shown in FIG. 2 that are 0.01λ apart;

FIG. 5 is a perspective view of a CSLA and associated ground plane, according to another embodiment of the present invention;

FIG. 6 is a plan view of a CSLA and associated ground plane, according to another embodiment of the present invention;

FIG. 7 is a plan view of a CSLA and associated ground plane, according to another embodiment of the present invention;

FIG. 8 is a graph with frequency on the horizontal axis and input reflection coefficients in dB scale on the vertical axis showing measured S₁₁ values for the CSLAs of the present invention;

FIG. 9 is a graph with time on the horizontal axis and time domain reflection coefficient on the vertical axis showing the time domain reflection coefficients of the CSLAs of the present invention;

FIG. 10 is a plan view of a CSLA and associated ground plane, where the CSLA has an oval configuration, according to another embodiment of the present invention;

FIG. 11 is a plan view of a CSLA and associated ground plane, where a portion of the sector has been removed and the CSLA has an oval configuration, according to another embodiment of the present invention;

FIG. 12 is a plan view of an E-shaped CSLA and associated ground plane, according to another embodiment of the present invention;

FIG. 13 is a graph with frequency on the horizontal axis and return loss on the vertical axis showing the measured return loss of the CSLA of FIG. 12;

FIG. 14 is a perspective view of a CSLA having overlapped antenna traces, according to another embodiment of the present invention;

FIG. 15 is a CSLA of the type shown in FIG. 14 including inductively loaded antenna traces, according to another embodiment of the present invention; and

FIG. 16 is a top view of a dual slot CSLA, according to another embodiment of the present invention.

DETAILED DESCRIPTION OF THE EMBODIMENTS

The following discussion of the embodiments of the invention directed to a two-sided overlapping coupled sectorial loop antenna is merely exemplary in nature, and is in no way intended to limit the invention or its applications or uses.

The equivalent circuit for a loop antenna, at its first resonance, is a shunt RLC circuit where the resistance represents the ohmic loss in the loop and the radiation resistance. The equivalent circuit parameters in general are functions of frequency. The variation of the capacitance as a function of frequency determines whether it is possible to control the spectral variation of the equivalent circuit inductance in such a way that a resonance condition is satisfied over a wide range of frequencies.

FIG. 1 shows a narrow-band sectorial loop antenna (SLA) 10 including an arch 12 and two pie-slice shaped sectors 14 and 16, according to an embodiment of the present invention. An AC feed 18 feeds the two sectors 14 and 16. The input impedance Z_s of the SLA 10 is a function of three geometrical parameters R_in, R_out and α, where R_in is the inner radius of the arch 12, R_out is the outer radius of the arch 12 and α is the arc angle in degrees of the sectors 14 and 16. The SLA 10 has a resonance behavior that is inductive below and capacitive above a first resonance.

Although not particularly shown in some of the several of the embodiments discussed herein for clarity purposes, the various arches and sectors of the sectorial loop antennas are metallized layers on a suitable dielectric substrate, as will be appreciated by those skilled in the art.

One way of controlling the self-impedance of the SLA 10 is by introducing an adjacent SLA with sufficient mutual coupling. This can be accomplished by connecting two identical SLAs 20 and 22 in parallel, as shown in FIG. 2. In this application, a single AC feed 24 feeds all four of the sectors of the SLAs 20 and 22. In this case, because of the symmetry, the input currents I₁ and I₂ are equal, but the direction of the magnetic field of the SLA 20 is in the opposite direction of the magnetic field of the SLA 22. Therefore, the magnetic flux of the SLAs 20 and 22 can be linked to provide a strong mutual coupling. The geometrical parameters can be varied to control the mutual coupling as a function of frequency.

For the two-port system of the SLAs 20 and 22, the following equations can be provided: V₁=Z₁₁I₁+Z₁₂I₂  (1) V₂=Z₂₁I₁+Z₂₂I₂  (2) Where V₁, I₁, V₂ and I₂ are the voltages and currents at the input ports of the SLA 20 and the SLA 22, respectively. Z₁₁ (Z₂₂) is the input impedance of the SLA 20 (22) in the presence of the SLA 22 (20) when it is open circuited. Z₂₁ and Z₁₂ represent the mutual coupling between the SLAs 20 and 22. Reciprocity mandates Z₁₂=Z₂₁ and the symmetry requires that Z₁₁=Z₂₂.

FIG. 3 is a CSLA 26 that includes the SLAs 20 and 22 coupled in parallel, according to the invention. In the CSLA 26, V1=V2 and, as a consequence of symmetry, I₁=I₂=I. The CSLA 26 includes two pie-slice shaped sectors 28 and 30 and two arches 32 and 34, where the sector 28 is a combination of two of the sectors of the SLAs 20 and 22, the sector 30 is a combination of the two other sectors of the SLAs 20 and 22, the arch 32 is the arch of the SLA 20 and the arch 34 is the arch of the SLA 22. The CSLA 26 is fed by an AC source 36 at the points of the sectors 28 and 30.

The input impedance of the CSLA 26 can be obtained from: $\begin{array}{cc}{Z}_{\mathrm{in}}=\frac{1}{2}\left(Z_{11}+Z_{12}\right)& \left(3\right)\end{array}$

In order to achieve a wideband operation, spectral variations of Z₁₁ and Z₁₂ must counteract each other. That is, when the real (imaginary) part of Z₁₁ increases with frequency, the real (imaginary) part of Z₁₂ should decrease so that the average impedance remains constant. This can be accomplished by optimizing the geometrical parameters of the antenna system. Z₁₁ and Z₁₂ are obtained by calculating the self and mutual impedances of the SLAs 20 and 22 using full-wave FDTD simulations.

FIGS. 4(a)-4(j) show the real and imaginary parts of Z₁₁ and Z₁₂ for the CSLAs 20 and 22 and the input impedance of the CSLA 26 as defined by equation (3), where R_in=13 mm and R_out=14 mm, for different values of α when they are placed at a distance of d=0.01λ_max apart, and where λ_max is the wavelength of the lowest frequency of operation. Particularly, FIGS. 4(a), (c), (e), (g) and (i) show the real part for α=5°, 20°, 40°, 60° and 80°, respectively, and FIGS. 4(b), (d), (f), (h) and (k) show the imaginary part for α=5°, 20°, 40°, 60° and 80°, respectively. The line 38 is the self-impedance, the line 40 is the mutual impedance and the line 42 is the input impedance as defined by equation (3). The graph lines show that as C/λ increases, the variations in the imaginary parts of Z₁₁ and Z₁₂ counteract each other for 1.5<C/λ<4 and the variations in the real parts of Z₁₁ and Z₁₂ counteract each other for 2<C/λ<3, where C=2πR_out. This suggests that the bandwidth of the CSLA 26 may be enhanced by choosing a in the range of 20°<α≦80°.

The optimum geometrical parameters of the CSLA 26 can be determined by an experimental sensitivity analysis. The three parameters that affect the response of the CSLA 26 are the inner radii R_in of the arches 32 and 34, the outer radii R_out of the arches 32 and 34 and the arc angle α. The lowest frequency of operation is determined by the overall effective circumference of the SLA 10 as: $\begin{array}{cc}{f}_1=\frac{2c}{\left(\pi -\alpha +2\right)\sqrt{{\varepsilon }_{\mathrm{eff}}}\left(R_{\mathrm{in}}+R_{\mathrm{out}}\right)}& \left(4\right)\end{array}$ Where ∈_eff is the effective dielectric constant of the antenna surrounding medium and c is the speed of light.

Choosing the lowest frequency of operation, the average radius R_av=(R_in+R_out)/2 of the CSLA 26 can be determined from equation (4). Therefore the parameters that remain to be optimized are α and τ=(R_out−R_in). In order to obtain the optimum value of α, nine different antennas with α values ranging from 5° up to 80° with R_in=13 mm and R_out=14 mm were fabricated and their S₁₁ as a function of frequency was measured. It has been discovered that the optimum value of α=60° results in the maximum impedance bandwidth for the CSLA 26.

Because the antenna topology of the CSLA 26 needs a balanced feed, half of the CSLA 26 along a plane of zero potential over a ground plane fed by a coaxial cable can be used. FIG. 5 is a plan view of a CSLA 44 including a ground plane 46, a pie-slice shaped sector 48 having its point positioned proximate the ground plane 46, a first arch 50 coupled to the ground plane 46 and one side of the sector 48 opposite to the point, and a second arch 52 coupled to the ground plane 46 and an opposite side of the end of the sector 48 from the point. A feed 54 feeds the point of the sector 48. In one embodiment, the feed 54 is a coaxial cable including an inner connector electrically coupled to the point of the sector 48 and an outer conductor electrically coupled to the ground plane 46. In this non-limiting embodiment, the CSLA 44 is fabricated using printed circuit technology on a thin dielectric substrate having a dielectric constant of ∈_r=3.4, a length of 3 cm, a width of 1.65 cm and a thickness of 500 μm and is mounted on a 10 cm×10 cm ground plane.

The next step in the optimization process of the CSLA 44 is to find the optimum value of the arch thickness τ=R_out−R_in. This is accomplished by providing the CSLA 44 with α=60°, R_av=13.5 mm and three different arch thicknesses of τ=0.4, 1.0 and 1.6 mm. It is observed that a thinner arch provides a wider bandwidth. For the thinnest value of τ=0.4 mm, a CSLA with a bandwidth of 3.7 GHz to 11.6 GHz is obtained.

The dimensions of CSLA 44 can be scaled in wavelength to achieve an arbitrarily different frequency band of operation. In one embodiment, the optimum geometrical parameters of the CSLA 44 include R_in=27.8 mm, R_out=28 mm and α=60°. Also, in one embodiment, the CSLA 44 is mounted on a 20 cm×20 cm ground plane, although the size of the ground plane is arbitrary. The dimensions are increased to lower the lowest and highest frequencies of operation and simplify the radiation pattern measurements. The CSLA 44 has a VSWR lower than 2.1 from 1.78 GHz to 14.5 GHz, which is equivalent to an 8.5:1 impedance bandwidth, when R_in is 27.8 mm, R_out is 28 mm and α=60°, and where the CSLA 44 is fabricated on the end piece of a dielectric substrate having a length of 6 cm, a width of 3 cm, a thickness of 500 μm and ∈_r is 3.4. Also, the gain and radiation patterns of the CSLA 44 across the frequency range of operation remain almost constant, particularly over the first two octaves of its impedance bandwidth.

The radiation patterns of the CSLA 44, in the azimuth plane, were measured across the entire frequency band. The radiation patterns remain similar up to about f=8 GHz. As the frequency increases beyond 8 GHz, the radiation patterns start having higher directivities in other directions.

The radiation patterns in the elevation planes were also measured for two principle planes at φ=0°, 180°, 0°≦θ≦180° and φ=90°, 270°, 0°≦θ≦180° at 2 GHz, 4 GHZ, 6 GHz, 8 GHz, 10 GHz, 12 GHz, 14 GHz and 16 GHz. As frequency increases, the electrical dimensions of the CSLA 44 increase, and thus, the number of lobes increases. Also, the number of minor sidelobes in the back of the ground plane (90°≦θ≦180°) increases significantly. This is caused by diffractions from the edge of the ground plane, which has very large electrical dimensions at higher frequencies.

At lower frequencies, the radiation patterns are symmetric. However, as the frequency increases, the symmetry is not observed very well. This is caused by the coaxial cable that feeds the CSLA 44 because it disturbs the symmetry of the measurements. Since the cable is electrically large at higher frequencies, a more pronounced asymmetry on the radiation patterns are observed at higher frequencies. In all of the measured radiation patterns, the cross polarization level (E_φ) is shown to be neglible. This is an indication of good polarization purity across the entire frequency band.

It is desirable to reduce the size and weight of the CSLA 44 by modifying its geometry. The CSLA 44 discussed above was optimized to achieve the highest bandwidth allowing variation of only two independent parameters. Size reduction is important for applications where the wavelength is large, such as ground penetrating radar or high frequency (HF) broadcast antennas. To examine the ways to reduce the size and weight of the CSLA 44, the current distribution over metallic surfaces of the CSLA 44 was calculated. The electric currents on the surface of the CSLA 44 can be computed using a full-wave simulation tool based on the method of moments.

It is noticed that the current magnitude is very small over a sector in the range of 0°≦θ≦30°. This suggests that this portion of the sector 48 of the CSLA 44 can be removed without significantly disturbing the current distribution of the CSLA 44.

FIG. 6 is a plan view of a CSLA 60 including a ground plane 66, where a portion 62 in the range of 0≦θ≦30° is removed from a coupled sector, such as the sector 48, to provide separated sectors 72 and 74. An arch 76 is coupled to the ground plane 66 and the sector 72 and an arch 78 is coupled to the ground plane 66 and the sector 74, as shown. In this non-limiting embodiment, the sectors 72 and 74 have an arc angle of 30° and the portion 62 has an arc angle of 60°. The CSLA 60 includes a coaxial connector 70 that a coaxial cable can be attached to, where an outer conductor 64 of the connector 70 is electrically coupled to the ground plane 66 and an inner conductor 68 of the connector 70 is electrically coupled to points of the sectors 72 and 74.

Applying the same approach and examining the current distribution reveals that the electric current density is larger around θ=30° and θ=60°, and has lower values in the area of 30°<θ<60°. Therefore, a section of the sectors 72 and 74 that is confined in the range 40°<θ<50° can be removed to obtain a CSLA 80 shown in FIG. 7. In the CSLA 80, like elements to the CSLA 60 are identified by the same reference numeral. In this embodiment, the insides of the pie-slice sections 82 and 84 are removed from the sectors 72 and 74, respectively, as shown.

The measured S11s of the CSLA 44, the CSLA 60 and the CSLA 80 are shown in FIG. 8, where graph line 90 is for the CLSA 44, graph line 92 is for the CSLA 60 and graph line 94 is for the CSLA 80. FIG. 8 shows that all of the CSLAs 44, 60 and 80 have VSRs lower than 2.2 in the frequency range of 2-14 GHz, as shown in Table 1 below. The best input match is, however, observed for the CSLA 60 with a VSWR lower than 2 across its entire band of operation.

TABLE 1
Antenna Type	Frequency Range	BW	Highest VSWR
CSLA 44	1.7-14.5 GHz	8.5:1	2.2
CSLA 60	2.14.7 GHz	7.35:1	2.2
CSLA 80	2.05-15.3 GHz	7.46:1	2.2

The CSLAs 44, 60 and 80 provide a very wide bandwidth. However, having a wideband frequency-domain response does not necessarily ensure that the CSLAs 44, 60 and 80 behave well in the time-domain, that is, a narrow time-domain pulse is not widened by the CSLAs 44, 60 and 80. Some multi-resonant wideband antennas, such as log-periodic antennas, due to multiple reflections within the antenna structure widen a narrow pulse in the time domain. Therefore, in order to ensure the usefulness of the CSLAs 44, 60 and 80 for time domain applications, the time-domain response of the CSLA must also be examined. FIG. 9 shows the time-domain variation of the reflection coefficient ρ of the CSLAs 44, 60 and 80. In FIG. 9, graph line 96 is for the CSLA 44, graph line 98 is for the CSLA 60 and graph line 100 is for the CSLA 80.

The CSLAs 44, 60 and 80 show the maximum reflection at t=0 ns, which corresponds to the discontinuity at the plane of calibration. The peak reflection at t=80 ps corresponds to the probe-antenna transition. The CSLA 60 has a similar behavior to the behavior of the CSLA 44. However, the CSLA 60 shows more small reflections. The increase in the number of small reflections is a consequence of the larger number of discontinuities in the antenna structure. In addition to the input reflection coefficient, transmission coefficients for two similar CSLAs were also measured.

The CSLAs 44, 60 and 80 all have a circular orientation, i.e., the arches and sectors define a portion of a circle. It may be desirable to reduce the height of the CSLA for certain applications, such as for a vehicle platform.

FIG. 10 is a plan view of a CSLA 110 depicting such an embodiment. The CSLA 110 includes an arch 112, an arch 114, a pie-slice shaped sector 116 and a ground plane 118. An outer conductor of a coaxial connector 120 is coupled to the ground plane 118 and an inner conductor of the coaxial connector 120 is coupled to the point of the sector portion 116. The orientation of the arches 112 and 114 and the sector portion 116 define an elliptical configuration, as depicted.

The elliptical orientation of the CSLA 110 can also be extended to the embodiment of the CSLA 60. Particularly, FIG. 11 is a plan view of a CSLA 124 including an arch 126, an arch 128, a first pie-slice shaped sector 130, a second pie-slice shaped sector 132, a ground plane 134 and a coaxial connector 136.

The arch angle α and R_in and R_out for the arches 112, 114, 126 and 128 can be those discussed above or other values for other applications, which may depend on the frequency band of interest. In one embodiment, the CSLAs 110 and 124 are about 4 m in length and about 1 m in height and are tuned to a VHF band of 20 MHz-90 MHz.

FIG. 12 is a plan view of a wide-band E-shaped double-loop antenna 140, according to another embodiment of the present invention. The antenna 140 includes a metal trace 142 printed on a dielectric substrate, where the metal trace 142 includes legs 144, 146 and 148, and a cross-bar 150. The legs 146 and 148 are electrically coupled to a ground plane 152, and the leg 144 is electrically coupled to a center conductor of a coax connector 154. An outer conductor of the connector is electrically coupled to the ground plane 152. The E-shaped double-loop antenna 140 provides an ultra-wide bandwidth similar to the CSLAs discussed above, but has a low profile and is lightweight.

FIG. 13 is a graph with frequency on the horizontal axis and measured return loss (S11) on the vertical axis showing the measured return loss of the antenna 140.

In order to reduce the length of the CSLA, arms of the antenna can be printed on two sides of a substrate and create an overlap between the arms. FIG. 14 is a perspective view of a two-sided overlapped CSLA 160 depicting this embodiment. The CSLA 160 includes a ground plane 162 and a dielectric substrate 164 mounted substantially perpendicular thereto. A first arm metal trace 166 is deposited on a first side 168 of the substrate 164 and a second arm metal trace 170 is deposited on an opposite side of the substrate 164. The arm traces 166 and 170 overlap at a center area 172 of the CSLA 160 to provide the reduced length. The metal traces 166 and 170 are connected to each other at feedline 174. The configuration of the metal traces 166 and 170 are deformed into a piece-wise linear manner to provide more degrees of freedom in the design including the height of the traces 166 and 170, the length of the traces 166 and 170 and the angle of the crossover portion 172 of the arm traces 168 and 170.

A resonant segment of a transmission line can be considered a resonant LC circuit. The length of the transmission line provides the inductance L. If an inductor is added to the end of the transmission line, it is possible to shorten the length of the line while maintaining the desired resonance. Therefore, the size of the CSLA 160 can be further reduced by adding inductors to the traces 168 and 170. A perspective view of a CSLA 180 is shown in FIG. 15 depicting this embodiment. Particularly, an inductor 182 is added to the end of the trace 170 opposite to the feedline 174, and an inductor 184 is added to the end of the trace 166 opposite to the feedline 174. Both lumped inductors and distributed inductors using printed loops can be used at the two sides of the substrate and connected therethrough by vias.

The several antennas discussed above have all been based on printed metal on a dielectric substrate. In an alternate embodiment, the various CSLAs discussed above can be based on slot antenna designs printed on a ground plane. FIG. 16 is a top view of a dual slot CSLA 190 illustrating this embodiment. The CSLA 190 includes a metallized ground plane 192 formed on a dielectric substrate. Pie-slice shaped portions 194 and 196 are removed from the ground plane 192, where a pie-slice shaped sector 198 is left within the portion 194 to be electrically isolated from the remaining portion of the ground plane 192, and a pie-shaped sector 200 is left in the pie-slice shaped portion 196 and is also electrically isolated from the remaining portion of the ground plane 192. The sectors 198 and 200 are fed by an AC source 202 at their points, as shown. The CSLA 190 provides the advantage of being conformal and can be printed on curved surfaces. Further, the CSLA 190 provides horizontal polarization. This can be particularly useful for polarimetric SAR systems, where two orthogonal antennas are required. The dual slot CSLA 190 can coexist with other CSLAs discussed above to provide both polarizations.

The foregoing discussion discloses and describes merely exemplary embodiments of the present invention. One skilled in the art will readily recognize from such discussion, and from the accompanying drawings and claims, that various changes, modifications and variations can be made therein without departing from the spirit and scope of the invention as defined in the following claims.

Claims

1. An antenna structure comprising: a ground plane; a feed; and an antenna including a substrate mounted to the ground plane, a first antenna trace formed on a first side of the substrate and a second antenna trace formed on a second side of the substrate, said first trace including a first end electrically coupled to the feed and a second end electrically coupled to the ground plane and said second trace including a first end electrically coupled to the feed and a second end electrically coupled to the ground plane.

2. The antenna structure according to claim 1 wherein the first ends of the first and second traces overlap on opposite sides of the substrate proximate the feed.

3. The antenna structure according to claim 1 further comprising a first inductor electrically coupled to the first trace proximate the second end of the first trace and a second inductor electrically coupled to the second trace proximate the second end of the second trace.

4. The antenna structure according to claim 3 wherein the inductors are lumped inductors.

5. The antenna structure according to claim 3 wherein the inductors are distributive inductors.

6. The antenna structure according to claim 1 wherein the feed is a coaxial feed having a center conductor electrically coupled to the traces and an outer conductor electrically coupled to the ground plane.

7. The antenna structure according to claim 1 wherein the substrate is a dielectric substrate.

8. The antenna structure according to claim 1 wherein the substrate is mounted to the ground plane substantially perpendicular thereto.

9. An antenna structure comprising: a feed; and an antenna including an antenna substrate, said antenna further including a first antenna trace deposited on a first side of the antenna substrate and a second antenna trace deposited on a second side of the antenna substrate where the first and second traces overlap at a center area and ends of the first and second traces are coupled to the feed at the center area.

10. The antenna structure according to claim 9 wherein the other ends of the first and second antenna traces are coupled to ground.

11. The antenna structure according to claim 10 wherein ground is a ground plane deposited on a ground substrate, and wherein the antenna substrate is mounted to the ground substrate substantially perpendicular thereto.

12. The antenna structure according to claim 9 further comprising a first inductor electrically coupled to the first trace and a second inductor electrically coupled to the second trace.

13. The antenna structure according to claim 12 wherein the inductors are lumped inductors.

14. The antenna structure according to claim 12 wherein the inductors are distributive inductors.

15. The antenna structure according to claim 9 wherein the feed is a coaxial feed having a center conductor electrically coupled to the traces and an outer conductor electrically coupled to ground.

16. A coupled sectorial loop antenna structure comprising: a substrate having a first side and a second side; a ground plane; a feed; a first sectorial loop antenna formed on the first side of the substrate, said first loop antenna including a first end coupled to the feed and a second end coupled to the ground plane; and a second sectorial loop antenna formed on the second side of the substrate, said second loop antenna including a first end coupled to the feed and a second end coupled to the ground plane.

17. The antenna structure according to claim 16 wherein the first ends of the first and second loop antennas overlap on opposite sides of the substrate proximate the feed.

18. The antenna structure according to claim 16 further comprising a first inductor electrically coupled to the first loop antenna proximate the second end of the first loop antenna and a second inductor electrically coupled to the second loop antenna proximate the second end of the second loop antenna.

19. The antenna structure according to claim 16 wherein the feed is a coaxial feed having a center conductor electrically coupled to the loop antennas and an outer conductor electrically coupled to the ground plane.

20. The antenna structure according to claim 16 wherein the substrate is mounted to the ground plane substantially perpendicular thereto.