# Patent

## Title
Directive, instantaneous wide bandwidth antenna

## Abstract

A directive, instantaneous wide bandwidth antenna is disclosed. The antenna can include a ground plane having a recess with a tapered region accessible by an electromagnetic field via a radiating aperture at a forward end of the recess. The antenna can also include an elongate dielectric feed disposed in the recess. The dielectric feed can have a tapered portion proximate the tapered region to guide the electromagnetic field into the recess through the radiating aperture and influence pattern directivity. The antenna can further include a conductive plating disposed at least partially about the dielectric feed in a wedge configuration to influence pattern beam width. The conductive plating can have a taper to facilitate propagation of the electromagnetic field over a range of frequencies. The conductive plating can be disposed toward a rearward end of the recess relative to the radiating aperture.

## Background
BACKGROUND
Antennas are utilized in a wide range of applications. Many applications drive ever-increasing antenna performance, such as higher gains and wider frequency bandwidths. High performance antennas are often found in vehicles, such as missiles or unmanned aerial vehicles (UAV).



BRIEF DESCRIPTION OF THE DRAWINGS
Features and advantages of the invention will be apparent from the detailed description which follows, taken in conjunction with the accompanying drawings, which together illustrate, by way of example, features of the invention; and, wherein:
FIG. 1A is an example illustration of a directive, instantaneous wide bandwidth antenna in accordance with an embodiment of the present invention.
FIG. 1B is an exploded view of the directive, instantaneous wide bandwidth antenna of FIG. 1A.
FIG. 2A is a detailed view of internal components of the directive, instantaneous wide bandwidth antenna of FIG. 1A.
FIG. 2B is an exploded view of the antenna internal components of FIG. 2A.
FIG. 3A is a perspective view of an elongate dielectric feed and conductive plating of the directive, instantaneous wide bandwidth antenna of FIG. 1A.
FIG. 3B is a side view of the elongate dielectric feed and conductive plating of FIG. 3A.
FIG. 3C is an exploded view of the elongate dielectric feed and conductive plating of FIG. 3A.
FIG. 4 is an end view of the conductive plating of FIG. 3A.



Reference will now be made to the exemplary embodiments illustrated, and specific language will be used herein to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended.
DETAILED DESCRIPTION
As used herein, the term “substantially” refers to the complete or nearly complete extent or degree of an action, characteristic, property, state, structure, item, or result. For example, an object that is “substantially” enclosed would mean that the object is either completely enclosed or nearly completely enclosed. The exact allowable degree of deviation from absolute completeness may in some cases depend on the specific context. However, generally speaking the nearness of completion will be so as to have the same overall result as if absolute and total completion were obtained. The use of “substantially” is equally applicable when used in a negative connotation to refer to the complete or near complete lack of an action, characteristic, property, state, structure, item, or result.
As used herein, “adjacent” refers to the proximity of two structures or elements. Particularly, elements that are identified as being “adjacent” may be either abutting or connected. Such elements may also be near or close to each other without necessarily contacting each other. The exact degree of proximity may in some cases depend on the specific context.
An initial overview of technology embodiments is provided below and then specific technology embodiments are described in further detail later. This initial summary is intended to aid readers in understanding the technology more quickly but is not intended to identify key features or essential features of the technology nor is it intended to limit the scope of the claimed subject matter.
Although prior antennas have been serviceable for many applications, such as missiles or UAVs, multiple antennas have sometimes been utilized in order to provide the desired bandwidth. In addition, use with missiles or UAVs also places size restrictions on antennas. For example, antenna depth and volume may be restricted to minimize the antenna's impact on aerodynamics, as well as to permit the antenna to fit within internal space constraints of the missile or UAV. In this case, using multiple antennas only compounds the size problem.
Accordingly, a directive, instantaneous wide bandwidth antenna is disclosed that increases instantaneous frequency bandwidth over previous antennas and can do so without requiring multiple antennas. In one aspect, the antennas of the present disclosure can be conformal to fit within a small size envelope, particularly at or near an outer surface of a missile or UAV. The directive, instantaneous wide bandwidth antenna can include a ground plane having a recess with a tapered region accessible by an electromagnetic field via a radiating aperture at a forward end of the recess. The antenna can also include an elongate dielectric feed disposed in the recess. The dielectric feed can have a tapered portion proximate the tapered region to guide the electromagnetic field into the recess through the radiating aperture and influence pattern directivity. The antenna can further include conductive plating disposed at least partially about the dielectric feed in a wedge configuration to influence pattern beam width. The conductive plating can have a taper to facilitate propagation of the electromagnetic field over a range of frequencies. The conductive plating can be disposed toward a rearward end of the recess relative to the radiating aperture.
One embodiment of a directive, instantaneous wide bandwidth antenna 100 is illustrated in FIGS. 1A and 1B. The antenna 100 can comprise a ground plane 110 having a recess 111 at a depth 119 with a tapered region 112 accessible by an electromagnetic field via a radiating aperture 113 at a forward end 114 of the recess 111. The aperture 113 can have a length 124 and the tapered region 112 can have a taper angle 123. The antenna 100 can also include an elongate dielectric feed 120 disposed in the recess 111. The elongate dielectric feed 120 can have a tapered portion 121 proximate the tapered region 112 of the recess 111 to guide the electromagnetic field into the recess 111 through the radiating aperture 113 and influence pattern directivity. The elongate dielectric feed 120 can be constructed of polytetrafluoroethylene (PTFE), ceramic, DUROID®, or any other low loss dielectric material having a relative dielectric constant of between about 2 and about 4.5. The antenna 100 can further include conductive plating 130 disposed at least partially about the dielectric feed 120 in a wedge configuration to influence pattern beam width. The conductive plating 130 can be constructed of copper, gold, silver, or any other suitable electrically conductive metallic material. As discussed in more detail hereinafter, the conductive plating 130 can also have a taper to facilitate propagation of the electromagnetic field over a range of frequencies. As shown in the figures, the conductive plating 130 can be disposed toward a rearward end 115 of the recess 111 relative to the radiating aperture 113. In one aspect, the conductive plating 130 can be covered by a conductive cover 140 disposed over a portion of the recess 111 and forming the radiating aperture 113. In another aspect, the tapered portion 121 of the dielectric feed 120 can be exposed through the radiating slot 113. The conductive cover 140 can be permanently affixed relative to the recess 111 or removably attached. The conductive cover 140 can be constructed of copper, gold, silver, or any other suitable electrically conductive metallic material.
The recess depth 119 can influence which frequencies the antenna 100 can receive. For example, a deeper recess depth 119 can facilitate the reception of lower frequencies and a shallower recess depth can facilitate the reception of higher frequencies. Altering the recess depth 119 can therefore result in a frequency shift. Indeed, in general, scaling the antenna 100 to have larger dimensions will facilitate the reception of lower frequencies and scaling the antenna 100 to have smaller dimensions will facilitate the reception of higher frequencies. In one aspect, the recess depth can be between about 2.5 mm and about 25 mm. In some embodiments, the taper angle 123 can be based upon the recess depth 119 and the length 124 of the aperture 113. Thus, in a particular aspect, the taper angle 123 can be given by the arctangent of the recess depth 119 divided by the aperture length 124.
In some embodiments, the antenna 100 can be conformal in that the antenna can have a low profile to fit, for example, at or near a surface of a missile or rocket. The conformal nature of such embodiments can accommodate missiles or rockets having interiors tightly packed with electronics, guidance, sensors, warheads, or other missile components by minimizing intrusion into precious interior space without protruding from the missile or rocket exteriors. The overall size dimensions of the antenna 100 can generally reflect the size dimensions of the ground plane 110, which can be designed as a structural support for the various antenna 100 components discussed herein. As such, the ground plane dimensions can be influenced by the size of the antenna components, some of which are discussed hereinafter. For example, ground plane thickness 101 can be slightly more than the recess depth 119 sufficient to provide structural support. The dielectric feed 120 and conductive plating 130 can guide electromagnetic fields to radiating aperture 113. As discussed further hereinafter, the angle of the wedge configuration, coupled with the relative dielectric constant of the dielectric feed material, can provide a highly directive antenna (very high front to back gain ratio). This also allows the antenna 100 to use a very shallow cavity depth, which can be important for most conformal antennas used in missile applications. For example, a small thickness 101 can be useful for small diameter missile applications. Antenna 100 dimensions can be optimized to allow the antenna 100 to perform better at any subset of frequencies from VHF to K band. In one aspect, the size of the antenna components can yield a thickness 101 of the antenna 100 of between about 3 mm and about 35 mm. For example, a thickness 101 of about 6.3 mm can result from an antenna optimized for X band frequencies.
As shown herein, the antenna 100 can provide very wide bandwidth, high directivity, and linear polarization in a shallow conformal package. In some embodiments, the antenna 100 can be implemented as a high gain conformal antenna that can be used in a very shallow cavity on a wide range of missile and UAV airframes. The extremely wide broadband frequency of operation can minimize fabrication tolerance issues and allow a single antenna 100 to be used in place of multiple narrow band antennas, thus reducing cost and volume required on tightly packaged missile or UAV systems. In one aspect, the antenna 100 can be used as a single antenna element or in an array of elements forming a larger antenna.
Performance of the antenna 100 is largely ground plane independent. Thus, the ground plane 110 can extend any suitable distance from the radiating aperture 113 of the recess 110 although, in general, a greater forward length 102 can lead to better antenna performance. In addition, the antenna 100 can be frequency scalable in that the antenna can be operable with a desired frequency range simply by physically scaling the antenna. For example, an antenna can be operable with higher frequencies by reducing the size of the antenna. In one aspect, the antenna 100 can be optimized for any subset of an entire frequency band or scaled to achieve higher or lower frequencies. In some embodiments, the antenna 100 can also exhibit monotonically increasing gain with frequency and a very stable gain curve above 2 GHz.
With reference to FIGS. 2A and 2B, and continued reference to FIGS. 1A and 1B, the antenna 100 can include an electromagnetic field absorber disposed in the recess 111. For example, absorber 150a, 150b, 150c can comprise a non-magnetic material, such as a carbon loaded foam or other lossy foam material, disposed to a side of the elongate dielectric feed 120 to minimize interference from electromagnetic scattering off a side wall 116a, 116b of the recess 111 while allowing forward or backward directed electromagnetic energy in the recess 111. In one aspect, the absorber can have a tapered portion 151a, 151b disposed proximate the tapered region 112 of the recess 111 in the radiating aperture 113. In another aspect, the absorber 150a, 150b, 150c can include portions disposed lateral to the conductive plating 130, for example, by having portions disposed proximate the side walls 116a, 116b of the recess 111. In a particular aspect, the absorber 150a, 150b can be spaced at a lateral distance 103a, 103b from the dielectric feed 120 to facilitate electromagnetic radiation therebetween. In one aspect, the lateral distance 103a, 103b can be selected to allow radiation to occur without absorbing power.
As shown in FIGS. 1A and 1B, a spacer 170a, 170b can be disposed between the absorber 150a, 150b, respectively, and the dielectric feed 120 to maintain the lateral distance 103a, 103b between the absorber 150a, 150b and the dielectric feed 120. The spacer 170a, 170b has been omitted from FIGS. 2A and 2B to reveal other characteristics and elements of the antenna 100. The spacer 170a, 170b can be constructed of a structural foam, such as ROHACELL®, polymethacrylimide, or any other low density rigid foam or other suitable material. In one aspect, the spacer can be constructed of a material having electrical properties that are similar to air.
As shown in the figures, the absorber 150a, 150b, 150c and the spacer 170a, 170b can be used to substantially fill space in the recess 111 between the side walls 116a, 116b. This can be beneficial to stabilize or prevent relative movement of antenna components during use, for example, on a missile or rocket. However, it should be recognized that the spacer 170a, 170b can be omitted or the absorber 150a, 150b, 150c can be designed to minimize material, thus resulting in empty space within the recess 111. In one aspect, regardless of whether a spacer 170a, 172b is included, a width 108a, 108b of the absorber 150a, 150b can be determined by the degree to which reflections from the side walls 116a, 116b are to be prevented or blocked.
With further reference to FIGS. 1A-2B, the antenna 100 can also include an absorber 160a, 160b comprising a magnetic material, such as ECCOSORB®, a radar absorbing material, or any other lossy magnetic load material, disposed toward the rearward end 115 of the recess 111 relative to the elongate dielectric feed 120 to minimize electromagnetic scattering off a back wall 117 of the recess 111. The absorber 160a, 160b can be tapered narrower toward the forward end 114 to influence broadband termination. A longer taper can provide more effective broadband termination, which can improve broadband performance of the antenna 100.
With particular reference to the exploded view in FIG. 2B, the absorber 160a, 160b is shown illustrated as two separate absorbers to accommodate an electrical connection 180 coupling a connector 181 to the conductive plating 130. It should be recognized that the absorber 160a, 160b can comprise a single component or any number of individual components, as desired. For example, a single absorber 160a, 160b can include a groove or channel similar to groove 152 of absorber 150c to accommodate the electrical connection 180. The electrical connection 180 can comprise any suitable electromagnetic transmission line, such as a cable (e.g., coaxial cable), a stripline, a microstrip, a wire, or any other suitable electrical connection coupling the conductive plating 130 to the connector 181. As shown in FIG. 1B, the electrical connection 180 can extend through a hole 118 or other suitable feature in the ground plane in order to provide external access to the connector 181. In one aspect, the connector 181 can be located below or behind an antenna cavity of a missile or UAV, which can allow more freedom in integrating the antenna 100 into thin-walled missile or UAV airframes. For example, the antenna 100 can be fed from a bottom side or rear of the ground plane 110, which can provide an antenna 100 that is highly adaptable to different airframe configurations. Referring again to FIG. 2B, the conductive plating 130 can be electrically coupled to the electrical connection 180 via a circuit board 182. In one aspect, the circuit board 182 can provide stability and support for the conductive plating 130 and the dielectric feed 120.
FIGS. 3A-3C illustrate several isolated views of the elongate dielectric feed 120 and the conductive plating 130. With further reference to FIGS. 1A-2B, a length 104 of the dielectric feed 120 in the radiating aperture 113 can correspond to the length 124 of the aperture 113 (see FIG. 1A) and influence pattern directivity of the antenna 100, such that increasing length 104 can produce a more directive antenna pattern. For example, the antenna 100 can have a highly directive focused beam (front to back ratio  ̃25 dB at 18 GHz). In one aspect, the length 104 can be between about 13 mm and about 102 mm. Although the length 104 primarily controls pattern directivity, the length 104 can also provide additional control of beam width. The length 104 is shown as extending to the conductive plating 130 because, in general, the conductive plating does not extend into the radiating aperture 113 and therefore represents an edge of the aperture 113, such as defined by the conductive cover 140. In one aspect, the conductive plating 130 can extend to the rearward edge of the aperture 113. However, the conductive plating 130 can terminate at any point short of the aperture 113. In one aspect, the elongate dielectric feed 120 can have a height 122 that corresponds to the depth 119 of the recess 111 (see FIG. 1B).
The tapered portion 121 can guide electromagnetic fields into the recess 111 through the radiating aperture 113. In one aspect, the tapered portion 121 can have a taper angle 105 that corresponds to the taper angle 123 of the tapered region 112 of the recess 111 (see FIG. 1B). The conductive plating 130 can also include a taper 131 to facilitate propagation of the electromagnetic field over a range of frequencies, thus contributing to the broadband attributes of the antenna 100. For example, the antenna 100 can have a very wide instantaneous frequency bandwidth ( ̃25:1 bandwidth (or even between 15:1 and 25:1) based on a voltage standing wave ratio (VSWR) of 3:1), which is a much wider frequency bandwidth than available from typical missile antennas. In some embodiments, the very wide instantaneous frequency bandwidth can be greater than 15:1 bandwidth. In other embodiments the very wide instantaneous frequency bandwidth can be between 15:1 and 25:1 bandwidth. In still other embodiments, the instantaneous frequency bandwidth can be less than 18:1 bandwidth.
It is further contemplated in still other embodiments that the antenna can be configured to operate over narrower instantaneous frequency bandwidths. For example, the various components or elements of the antenna can be configured differently, such that the antenna can operate over narrower instantaneous frequency bandwidths. In some embodiments this may be 2:1 bandwidth. In other embodiments this may be from 2:1 up to the wider frequency bandwidths as discussed above.
In one aspect, a taper angle 106 of the conductive plating can be between about 9 degrees and about 10 degrees. Typically, the tapers discussed herein are linear, although other taper shapes, such as non-linear, are contemplated. In some aspects, the taper angle 106 of the taper 131 and a length 109 of the conductive plating 130 can influence pattern directivity of the antenna 100. These dimensions can be balanced or optimized with the length 104 of the dielectric feed 120 in the radiating aperture 113 to provide an antenna 100 with desired pattern directivity, pattern beam width, and frequency bandwidth. The antenna 100 as shown and described herein can therefore provide a wide instantaneous frequency bandwidth, such that the wide frequency bandwidth is always available and no tuning is needed in order to achieve the wide bandwidth.
It should be recognized that aside from the taper angle 105, the dielectric feed can be of any suitable shape or dimension. In some embodiments, a shape or dimension of the dielectric feed can be based on a shape or dimension of the conductive plating, such as wedge angle 107 shown in FIG. 4. In addition, although the conductive plating 130 is shown in the figures as being disposed external to the dielectric feed 120, it should be recognized that the conductive plating 130 can be disposed, in whole or in part, inside the dielectric feed 120. Thus, a shape of a dielectric feed in accordance with the present disclosure can vary widely from the figures discussed herein.
FIG. 4 illustrates an end view of the conductive plating 130. The conductive plating 130 can have a wedge configuration 132 with a wedge angle 107 influencing pattern beam width, such that decreasing the wedge angle 107 produces a narrower beam width. For example, the wedge angle 107 can provide control of the antenna pattern main lobe beam width. In one aspect, the wedge angle 107 can be between about 45 degrees and about 60 degrees. The conductive plating 130 disposed about a portion of the dielectric feed 120 can provide unique control over antenna beam width above C band, which exceeds the control over pattern beam width available from typical missile of UAV antennas. The conductive plating 130 can be of any suitable thickness. In one aspect, a plating thickness can be between about 0.02 mm and about 0.25 mm. The conductive plating 130 and the conductive cover 140 can be configured to be in electrical contact with one another. For example, a top portion 133 of the conductive plating 130 can be configured to electrically interface with a bottom of the conductive cover 140. In some embodiments, the conductive plating 130 can be configured without a top portion 133. In this case, sides 134a, 134b can be configured to electrically interface with a bottom of the conductive cover 140. In general, sides 134a, 134b can be substantially planar, although variations from a planar condition can exist with decreased antenna performance. In addition, although generically referred to herein as “plating,” the conductive plating 130 can be constructed or manufactured in any suitable manner using any suitable technique.
In accordance with one embodiment of the present invention, a method for facilitating use of a directive, instantaneous wide bandwidth antenna is disclosed. The method can comprise providing an antenna including a ground plane having a recess with a tapered region accessible by an electromagnetic field via a radiating aperture at a forward end of the recess, an elongate dielectric feed disposed in the recess, the dielectric feed having a tapered portion proximate the tapered region to guide the electromagnetic field into the recess through the radiating aperture and influence pattern directivity, and a conductive plating disposed at least partially about the dielectric feed in a wedge configuration to influence pattern beam width, and having a taper to facilitate propagation of the electromagnetic field over a range of frequencies, wherein the conductive plating is disposed toward a rearward end of the recess relative to the radiating aperture. Additionally, the method can comprise facilitating conformance of the antenna in an antenna cavity of a vehicle. In one aspect, a thickness of the antenna is thicker than a recess depth (e.g., see recess depth 119 of FIGS. 1A and 1B), and can be between about 3 mm and about 35 mm. It is noted that no specific order is required in this method, though generally in one embodiment, these method steps can be carried out sequentially.
It is to be understood that the embodiments of the invention disclosed are not limited to the particular structures, process steps, or materials disclosed herein, but are extended to equivalents thereof as would be recognized by those ordinarily skilled in the relevant arts. It should also be understood that terminology employed herein is used for the purpose of describing particular embodiments only and is not intended to be limiting.
Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present invention. Thus, appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment.
As used herein, a plurality of items, structural elements, compositional elements, and/or materials may be presented in a common list for convenience. However, these lists should be construed as though each member of the list is individually identified as a separate and unique member. Thus, no individual member of such list should be construed as a de facto equivalent of any other member of the same list solely based on their presentation in a common group without indications to the contrary. In addition, various embodiments and example of the present invention may be referred to herein along with alternatives for the various components thereof. It is understood that such embodiments, examples, and alternatives are not to be construed as de facto equivalents of one another, but are to be considered as separate and autonomous representations of the present invention.
Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the description, numerous specific details are provided, such as examples of lengths, widths, shapes, etc., to provide a thorough understanding of embodiments of the invention. One skilled in the relevant art will recognize, however, that the invention can be practiced without one or more of the specific details, or with other methods, components, materials, etc. In other instances, well-known structures, materials, or operations are not shown or described in detail to avoid obscuring aspects of the invention.
While the foregoing examples are illustrative of the principles of the present invention in one or more particular applications, it will be apparent to those of ordinary skill in the art that numerous modifications in form, usage and details of implementation can be made without the exercise of inventive faculty, and without departing from the principles and concepts of the invention. Accordingly, it is not intended that the invention be limited, except as by the claims set forth below.

## Claims

1. A directive, instantaneous wide bandwidth antenna, comprising:
a ground plane having a recess with a tapered region accessible by an electromagnetic field via a radiating aperture at a forward end of the recess;
an elongate dielectric feed disposed in the recess, the dielectric feed having a tapered portion proximate the tapered region to guide the electromagnetic field into the recess through the radiating aperture and influence pattern directivity; and
a conductive plating disposed at least partially about the dielectric feed in a wedge configuration to influence pattern beam width, and having a taper to facilitate propagation of the electromagnetic field over a range of frequencies, wherein the conductive plating is disposed toward a rearward end of the recess relative to the radiating aperture.

2. The antenna of claim 1, wherein the wedge configuration comprises a wedge angle of between about 45 degrees and about 60 degrees.

3. The antenna of claim 1, wherein the recess comprises a depth of between about 2.5 mm and about 25 mm.

4. The antenna of claim 1, wherein the taper of the conductive plating comprises a taper angle of between about 9 degrees and about 10 degrees.

5. The antenna of claim 1, wherein a length of the dielectric feed in the radiating aperture is between about 13 mm and about 102 mm.

6. The antenna of claim 1, further comprising a conductive cover disposed over a portion of the recess and forming the radiating aperture.

7. The antenna of claim 1, further comprising an electromagnetic field absorber disposed in the recess.

8. The antenna of claim 7, wherein the absorber comprises a magnetic material disposed toward the rearward end of the recess relative to the elongate dielectric feed to minimize electromagnetic scattering off a back wall of the recess.

9. The antenna of claim 8, wherein the absorber is tapered narrower toward the forward end to influence broadband termination.

10. The antenna of claim 8, wherein the magnetic material comprises a lossy magnetic load material.

11. The antenna of claim 7, wherein the absorber comprises a non-magnetic material disposed to a side of the elongate dielectric feed to minimize interference from electromagnetic scattering off a side wall of the recess while allowing forward or backward directed electromagnetic energy in the recess.

12. The antenna of claim 11, wherein the absorber comprises a tapered portion disposed proximate the tapered region of the recess in the radiating aperture.

13. The antenna of claim 11, wherein the absorber is disposed lateral of the conductive plating.

14. The antenna of claim 11, wherein the non-magnetic material comprises a lossy foam material.

15. The antenna of claim 11, wherein the absorber is spaced at a lateral distance from the dielectric feed to facilitate electromagnetic radiation therebetween.

16. The antenna of claim 15, further comprising a spacer disposed between the absorber and the dielectric feed to maintain the lateral distance between the absorber and the dielectric feed.

17. The antenna of claim 1, further comprising a circuit board, wherein the conductive plating is electrically coupled to the circuit board.

18. The antenna of claim 1, wherein a thickness of the antenna is between about 3 mm and about 35 mm.

19. A method for facilitating use of a directive, instantaneous wide bandwidth antenna, comprising:
providing an antenna including
a ground plane having a recess with a tapered region accessible by an electromagnetic field via a radiating aperture at a forward end of the recess,
an elongate dielectric feed disposed in the recess, the dielectric feed having a tapered portion proximate the tapered region to guide the electromagnetic field into the recess through the radiating aperture and influence pattern directivity, and
a conductive plating disposed at least partially about the dielectric feed in a wedge configuration to influence pattern beam width, and having a taper to facilitate propagation of the electromagnetic field over a range of frequencies, wherein the conductive plating is disposed toward a rearward end of the recess relative to the radiating aperture; and

facilitating conformance of the antenna in an antenna cavity of a vehicle.

20. The method of claim 19, wherein a thickness of the antenna is between about 3 mm and about 35 mm.