Exemplary embodiments of the present invention relate generally to a novel design for a compact, slot-loaded, proximity fed patch antenna structure. While the description herein describes frequency bands that are employed in global positioning system (GPS) implementations for exemplary calculations, the design may be equally applied to other applications where a compact, dual band antenna is desirable.
Global navigation satellite systems (GNSS) such as GPS have become very commonly used devices. Well known uses include automobile and truck navigation systems and military applications. The rapid growth of GNSS technology also includes a growing list of new applications, some examples of which include: vehicle and package tracking, child monitoring, surveying, construction, sports equipment, workforce management, and farming. Along with the growth of applications, there are a growing number of GNSS systems such as GPS (U.S.), GLONASS (Russia), Galileo (Europe), and Beidou (China). Due to this growth, additional frequency bands are being allocated for GNSS use. As a result, GNSS transmitting and receiving electronics, including antennas, may be required to be configurable for a range of frequency channels. There is also an increasing amount of clustering of GNSS channels within these bands. A direct result of this clustering is the need for advanced coding schemes for the satellite signals used by GPS devices, and these advanced coding schemes frequently require wider bandwidth GNSS transmission and reception systems.
In addition to being able to receive a greater number of GNSS channels and having wider channel bandwidths, many GNSS applications require antennas to be small in size in order to fit into the desired device packaging. For example, GPS currently operates using the L1 (1575 MHz) and L2 (1227 MHz) bands. Most existing commercial small L1/L2 GNSS/GPS antennas have relatively narrow 10 MHz bandwidths that are not adequate for supporting advanced GPS coding schemes. Bowtie dipole and spiral antenna designs have been used to achieve wider bandwidth but such designs are relatively large in size and not suitable for small GPS devices. Because of the increasing number of GNSS frequency bands, requirements for wider bandwidths, and a desire for small physical sizes, there is an unmet need for a dual-band, wide bandwidth, and small in size antenna design.
Disclosed herein is an exemplary antenna structure adapted to provide dual band coverage comprising a dielectric substrate layer and a patch layer configured with slots. An embodiment is also disclosed that further comprises a 90 degree hybrid coupler in electronic communication between the patch layer and the signal source feeding the patch layer. Embodiments of the antenna are adapted to utilize both patch and slot modes to produce wide bandwidth and dual band coverage. An additional embodiment of the invention is comprised of a plurality of antennas, each comprising a dielectric substrate layer, and a patch layer configured with slots. An exemplary embodiment may also include a 90 degree hybrid coupler in electronic communication between the patch layer and the signal source feeding the patch layer.
In addition to the novel features and advantages mentioned above, other benefits will be readily apparent from the following descriptions of the drawings and exemplary embodiments.
Exemplary embodiments of the present invention are directed to a compact dual band antenna design. For example, one embodiment of the antenna may be configured to be 25.4 mm in diameter and 11.27 mm in height (i.e., thickness). In one example, the size of the antenna is only about λ/10 in L2 band. Unlike known designs, exemplary embodiments of the present invention do not require stacked patch configurations and therefore, do not require an internal conducting patch. In an exemplary embodiment, dual band coverage may be achieved by operating the patch mode in L2 band and slot mode in L1 band.
Referring to
In an exemplary embodiment of the invention, at least two conducting strips may serve as proximity probes (i.e., feeds). As is illustrated in
Once upper and lower frequency bands are chosen based on the intended application, dielectric constants, the thickness of the upper and lower dielectric layers, the length and width dimensions of the meandering slots, and the length of the inner tuning stubs may be varied to achieve resonant frequencies at those upper and lower bands. An optimal design of the antenna structure illustrated in
The resonant frequency of the lowest mode may then be estimated from Equation 2, using the estimated ∈eff from Equation 1 and the chosen diameter (D).
If the top dielectric layer is fabricated from thermoset microwave laminate material as disclosed above then, in practice, the dielectric constant and thickness (∈1, h1) of the top dielectric layer may be determined based on available printed circuit board materials. Therefore, the characteristics of the ceramic puck material used to form the bottom dielectric layer may be used to produce a patch mode resonance that is close to the desired lower frequency band. The bandwidth requirement of the application to which the antenna structure will be applied may be used to determine the total thickness (h1+h2) of the stacked dielectric layers.
The second step is to determine the length (L) and width (W) of the meandering slots. The length is shown as 108 and the width as 110 in
The third step is to adjust the length of the inner tuning stubs, the outlines of which are defined by the conductive material. One such tuning stub is shown at 112 in
In an exemplary embodiment, a tuning slot stub may be adapted to be used for fine tuning a resonant frequency of L1 mode without affecting L2 mode.
An embodiment of the antenna device using the calculations and steps described above and illustrated in
In one example of performance, the measured reflection coefficient was less than −20 dB from 1.1 GHz to 1.7 GHz and the transmission coefficient was approximately −3.2 dB, very close to a desired −3 dB from a half power divider, within the frequency range of interest. In this example, the measured phase difference between the two output ports varied monotonically from 88° at 1.227 GHz to 90° at 1.575 GHz, which was suitable for CP operation.
In an exemplary embodiment, when the disclosed design steps are performed to design an embodiment of the invention optimized to operate at the GPS L1 and L2 bands using Rogers TMM10i board (h1=1.27 mm, ∈r=9.8, tan δ=0.002) as the upper dielectric layer and a high dielectric ceramic puck (h2=10 mm, ∈r=45, tan δ≈0.0001) as the lower dielectric layer, the resultant design parameters are as summarized in Table 1.
Other parameters may be obtained with the choice a different dielectric substrate. As is illustrated in
In an exemplary embodiment, the resonant field distribution may occupy substantially the entire substrate in L2 (1227 MHz) mode and be mostly concentrated around the meandered slots in L1 (1575 MHz) mode. The meandered slots, the center circular hole of the patch, and the high dielectric substrate may help to establish L2 mode resonance within a physically small antenna volume. The concentration of fields only around slots in L1 band may also make it possible to tune the L1 frequency independently by adjusting the length I3 of the inner tuning slot stubs.
A known difficulty with closely space antenna array elements is the impact that such an array may have on the impedance matching, resonant frequency, and radiation pattern of elements of the array. Exemplary embodiments of the invention have been found to exhibit minimal impact when arranged in a compact array configuration (e.g., a compact 4-element array configuration).
In one example, an embodiment of an array configuration was designed for operation at 1.227 GHz with 45 MHz 3-dB bandwidth and 1.575 GHz with 50 MHz 3-dB bandwidth at zenith. Such an example may be miniaturized down to 25.4 mm in diameter without the feeding network and approximately 25.4 mm by 40.6 mm with the feeding network. Simulation of such an example has resulted in an indication that 90% radiation efficiency may be achieved using low loss dielectric material. In another exemplary embodiment, RHCP feeding circuitry may be implemented using a small 0°-90° hybrid chip that provides desired power splitting and stable quadrature phase difference at its two outputs. The measured gain and pattern data of such an embodiment validated the simulated performance and showed wide RHCP sky coverage and more than 15 dB of RHCP to left hand circular polarization (LHCP) isolation at both L1 and L2 bands. Other embodiments are possible based on the teaching provided herein. For example, some embodiments may have a diameter less than about 25.4 mm (i.e., 1 inch) and/or a height less than about 11.27 mm. Other embodiments may have greater dimensions.
Such as described, exemplary embodiments may employ a low-loss, high-dielectric substrate and the meandered-slot designs to increase the antenna's electrical size. An example of the design may also adopt external proximity probes. In an exemplary embodiment, the patch mode and the slot mode may share the probe(s). The combination of the above features greatly improves manufacturability and reliability. In addition, an example of the design may utilize a small 0°-90° hybrid chip (e.g., Mini-circuit QCN-19) to reduce the size of feeding network and achieve good RHCP performance over a wider frequency range. In one example, the antenna may be adapted to provide RHCP by combining two orthogonal modes via the hybrid chip. As a further example, the antenna design may be applied in an array (e.g., 4 elements) without suffering performance degradation due to mutual coupling. For example, in one such an embodiment, the antennas may have separate connectors such that one can combine received signals (digitally in post processing) using different algorithms to improve received signal quality and/or to suppress interference.
Any embodiment of the present invention may include any of the optional or preferred features of the other embodiments of the present invention. The exemplary embodiments herein disclosed are not intended to be exhaustive or to unnecessarily limit the scope of the invention. The exemplary embodiments were chosen and described in order to explain the principles of the present invention so that others skilled in the art may practice the invention. Having shown and described exemplary embodiments of the present invention, those skilled in the art will realize that many variations and modifications may be made to the described invention. Many of those variations and modifications will provide the same result and fall within the spirit of the claimed invention. It is the intention, therefore, to limit the invention only as indicated by the scope of the claims.
This application claims priority to U.S. Provisional Application No. 61/668,633, filed Jul. 6, 2012, which is hereby incorporated by reference in its entirety.
This invention was made with government support under contract no. FA8650-09-C-1608 awarded by Air Force SBIR Phase II. The government has certain rights in the invention.
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