This disclosure relates to reconfigurable electro-magnetic (EM) apertures and in particular to pixelated reconfigurable antennas.
Reconfigurability of an electro-magnetic (EM) surface is often desired when a variety of RF functions are needed and there is a space or weight limitation at the location on which the electromagnetic structure is to be mounted. Reconfigurability of an EM surface can also save assembly time and material costs of having to swap out RF apertures when a new RF application is needed.
J. D. Wolfm N. P. Lower, L. M Paulsen, J. P. Doene, and J. B. West describe, in “Reconfigurable radio frequency (RF) surface with optical bias for RF antenna and RF circuit applications”, U.S. Pat. No. 7,965,249, issued Jun. 21, 2011, a reconfigurable antenna with optical actuation of photoconductive switches between small metallic patches forming a pixelated surface. Light emitting diodes (LEDs) are used to actuate the photoconductive switches, which has the disadvantage of requiring constant power input to drive the LED's to keep the switches closed. In a large EM structure very high power would be required. Lacking in the description is any teaching on what happens to an RF feed when the antenna is reconfigured
L. Zhouyuan, D. Rodrigo, L. Jofre, and B. A. Cetiner, in “A new class of antenna array with a reconfigurable element factor,” IEEE Trans. Antenna Propagation., Vol. 61, No. 4, April 2103, pp. 1947-1955 describe a reconfigurable element that uses a parasitic pixel array of small metallic patches which are reconfigured using switches to provide beam steering or polarization switching. A non-reconfigurable patch antenna is used as the driver for the parasitic pixels, which limits the bandwidth to the patch size.
Other examples of pixelated structures for reconfigurable antennas are described by E. K. Walton, and B. G. Montgomery, in “Reconfigurable antenna using addressable pixel pistons,” U.S. Pat. No. 7,561,109, issued Jul. 14, 2009; E. Rodrigo and L. Jofre, in “Frequency and radiation pattern reconfigurability of a multi-size pixel antenna,” IEEE Trans. Antenna Propagation., Vol. 60, No. 5, May 2012, pp. 2219-2225; and A. G. Besoli and F. De Flaviis, in “A multifunction reconfigurable pixeled antenna using MEMS Technology on printed circuit board,” IEEE Trans. Antennas and Propagation, Vol. 59, No. 12, Dec. 2011. However, all of these use mechanical or electronic switches which require a complicated and RF degrading direct current (DC) bias network.
What is needed is an improved reconfigurable electromagnetic surface. The embodiments of the present disclosure answer these and other needs.
In a first embodiment disclosed herein, a reconfigurable electro-magnetic tile comprises a laser layer comprising a plurality of lasers, and a pixelated surface comprising a plurality of metal patches and a plurality of switches, wherein each respective switch of the plurality of switches is in a gap between a first respective metal patch and a second respective metal patch, wherein each respective switch is optically coupled to at least one respective laser of the plurality of lasers, wherein each switch of the plurality of switches comprises a phase change material, wherein the phase change material of a respective switch changes from a non-conducting state to a conducting state when the coupled respective laser lases a first power density of light on the phase change material of the respective switch, and wherein the phase change material of a respective switch changes from a conducting state to a non-conducting state when the coupled respective laser lases a second power density of light on the phase change material of the respective switch.
In another embodiment disclosed herein, a method of providing a reconfigurable electro-magnetic tile comprises providing a laser layer comprising a plurality of lasers, and providing a pixelated surface comprising a plurality of metal patches and a plurality of switches, wherein each respective switch of the plurality of switches is in a gap between a first respective metal patch and a second respective metal patch, wherein each respective switch is optically coupled to at least one respective laser of the plurality of lasers, wherein each switch of the plurality of switches comprises a phase change material, wherein the phase change material of a respective switch changes from a non-conducting state to a conducting state when the coupled respective laser lases a first power density of light on the phase change material of the respective switch, and wherein the phase change material of a respective switch changes from a conducting state to a non-conducting state when the coupled respective laser lases a second power density of light on the phase change material of the respective switch.
These and other features and advantages will become further apparent from the detailed description and accompanying FIG.s that follow. In the FIG.s and description, numerals indicate the various features, like numerals referring to like features throughout both the drawings and the description.
In the following description, numerous specific details are set forth to clearly describe various specific embodiments disclosed herein. One skilled in the art, however, will understand that the presently claimed present disclosure may be practiced without all of the specific details discussed below. In other instances, well known features have not been described so as not to obscure the present disclosure.
The present disclosure describes an electromagnetic (EM) tile 10, as shown in
An integrated reconfigurable electromagnetic tile 10 has radio frequency (RF) and optical layers with interconnecting RF feed lines 16 that can be placed with other reconfigurable electromagnetic tiles 10 to form a larger reconfigurable electromagnetic surface. The electromagnetic pixelated tile 10 has metallic patches 32, which have dimensions that are much smaller than a wavelength for a desired radio frequency of operation. Each metal patch 32 may be considered a pixel 32 in the electromagnetic pixelated tile 10. There are a limited number, much less than the number of pixels 32, of non-reconfigurable RF feed structures 16 which connect transmit/receive modules 12 to the pixelated surface for RF feeding of the various electromagnetic structures. An RF switch fabric has a PCM switch matrix of PCM switches 34 between the pixels 32 with an overlaying fine granulated array of sub-wavelength metallic pixels 32. The RF switches 34 allow the electromagnetic pixelated tile 10 to be reconfigured into a multitude of electromagnetic functions. The RF switches 34 can be optically actuated and reset using a VCSEL array 14. The vertical-cavity surface-emitting laser (VCSEL) array 14 has an array of semiconductor laser diodes with laser beam emissions perpendicular from the top surface, rather than conventional edge-emitting semiconductor lasers. Because VCSELs emit the beam perpendicular to the active region of the laser as opposed to parallel as with an edge emitter, an array of VCSELs can be processed simultaneously, such as on a Gallium Arsenide wafer. A control network, examples of which are shown in
Some advantages of present disclosure are a switch fabric with PCM switches 34 that latch so that no standby power is needed, on state resistance as low as ˜0.3Ω, enabling low RF loss (˜0.1 dB), fast switching—RF switch speed figure-of-merit (1/(2πRonCoff)) of 20 THz, high on/off ratio →104 which provides high isolation (˜20 dB), ultra-linearity IP3 ˜ζdBm, high power handling—10 W, and robustness—only need a passivation layer. In the prior art using semiconductor and RF MEMS switches, bias lines are required for actuation resulting in significant electromagnetic interference. RF MEMS switches and MEMS piston switches are mechanical and may require hermetic packaging for robustness, semiconductor and MEMS switches usually require constant source application, and thus standby power. Furthermore, semiconductor and some material based switches may be nonlinear under high power transmission.
The reconfigurable pixelated surface tile 30 may have reconfigurable non-driven antenna elements and other circuits between driven antenna elements of the array. Electromagnetic coupling between the driven and non-driven elements allows a grating lobe free beam scan, because the driven and coupled elements can have >λ/2 spacing. This allows reduction of T/R module count by factor of 4 or more. Reconfiguration occurs only on one surface and non-reconfigurable RF feed lines simplify integration. Sub-wavelength pixels allow frequency reconfigurability and beam scanning.
In the prior art, conventional arrays use a transmit/receive (T/R) module per radiation element for maximum scan angles. Reconfiguration of antenna elements requires reconfigurable RF feeds to prevent grating lobes. Some switch technologies may require larger pixels and thus reduce the ability to fine tune frequency or beam scanning.
The ultrafast optical actuation of the switches 34 by VCSEL array 14 has the following advantages. Laser bias lines are below the wideband multilayer ground plane 22, which shields the patches 32 from any radio frequency (RF) interference from the potentially thousands of control lines for the lasers. Energy is focused and the switches can turn on and off in ˜10 ns to 100 ns, because separate heater elements with their associated thermal time constant are not required. Also, laser array actuation of the PCM switches 34 is very power efficient compared to light emitting diode (LED) actuation of photo conductive switches, which would require constant power.
In the present disclosure a wideband multilayer ground plane 22 can change the effective antenna array ground plane location with frequency, which mitigates the change in bandwidth (BW) vs. frequency. The use of a non-reconfigurable ground plane but wideband ground plane 22 simplifies integration. In the prior art, use of a single metallic ground plane causes the array bandwidth to vary with frequency. A disadvantage of a reconfigurable ground plane is that switches would be needed in the ground plane layer.
In the present disclosure, heterogeneous wafer integration may be used to form tiles with micron level control of proximity and alignment. The wafer scale integrated microsystem takes advantage of the inherent accuracy of microfabrication methods for patterning, bonding and thinning to construct the tiles. Parallel fabrication of sub-tiles allows independent optimization of sub-layer functions, e.g., PCM switches 34, VCSELS 14 and micro lenses 20 and 26 prior to integration. A non-integrated approach for optics would require a much larger system and more power, and a component assembly approach would not provide the alignment accuracy required to focus optical power, have higher power consumption, and would be less efficient.
The bottom layer has transmit/receive T/R modules 12 that condition the RF signal for transmitting and receiving. These T/R modules 12 typically consist of power amplifiers, low-noise amplifiers, mixers, phase shifters, switches, and circulators. Fewer of the T/R modules 12 are required over prior art approaches, because reconfigurability of the surface pixels 32 means that non-driven element tuning can be used to do beam steering, impedance matching, filtering, etc.
The next layer up is the array of vertical cavity surface emitting lasers (VCSELs) 14. These lasers 14 provide the controlling optical signal that actuate or reset the switches 34 between each pixel 32 of the tile 10. There are one or more lasers 14 for each pixel 32. Each VCSEL 14 has control electronics, examples of which are shown in
In order to focus the light from the VCSELs at the reconfigurable surface, one or more micro lens arrays are used. If more than one micro lens array is used, then the lens layers may not be contiguous and may appear at different level layers in the tile, such as shown in
The RF non-reconfigurable ground plane 22 has small holes 23 or pin holes having a diameter much less than an RF wavelength for a desired radio frequency of operation, to allow transmission of light from the lasers 14. Since the ground plane 22 is non-reconfigurable, in order to cover a wide bandwidth, the ground plane 22 has a multiple-layer frequency selective reflector, which is well known to persons skilled in the art. A multiple-layer frequency selective reflector is a frequency selective surface and may consist of arrays of conducting elements on or between layers of dielectric substrates with band pass or band stop characteristics. Reference [1] below describes one example of such a multiple-layer frequency selective reflector, and is incorporated herein as though set forth in full. The ground plane 22 may also be connected to an overall system ground.
A substrate 24 may be between the ground plane 22 and the micro lens layer 26. The substrate should be optically transparent to allow the optical switch actuation signals to be transmitted through the substrate with minimum attenuation. The substrate 24 may be glass, fused silica, quartz, air, or other optically transparent plastics. Also, for VCSELs 14 that operate in the infrared spectrum, other substrates, such as GaAs could be used.
The pixelated surface tile 30 is the layer that consists of an arrangement of metal patches 32 and switches 34. The metal patches 32 may be various shapes including square, rectangular or octagonal, of dimension much less than a wavelength. The pixelated surface tile 30 has a substrate with the metal patches 32 and switch 34 on the substrate. The substrate for reconfigurable pixelated surface tile 30 may also be optically transparent for transmission of the optical switch actuation signals. The switches 34 are in the gaps between the patches 32, and are preferably of phase change material (PCM). These PCM switches 34 are directly above one or more VCSELS 14 such that the light from a VCSEL 14 is focused upon the PCM material 34. A close-up detail of a few patches 32 and PCM switches 34 is shown in the
RF input lines 16 connect the transmit/receive module layer 12 to a patch 32 on the reconfigurable pixelated surface tile 30. The number of RF lines is dependent upon the minimum and maximum frequencies of operation, the tile size, and the resolution obtainable from the pixels. Once the number of RF lines are determined for an application, the RF input lines 16 are non-reconfigurable. An RF signal can be connected to a reconfigurable EM structure on the reconfigurable pixelated surface tile 30 by configuring a transmission line from the patch 32 to which an RF input line 16 is connected by appropriate actuation of the PCM switches 34. In addition, non-reconfigurable RF ground lines 25 may be fabricated from the RF ground plane 22 to a patch on the reconfigurable pixelated surface tile 30. These ground lines could serve as an RF ground for reconfigurable transmission line elements on the reconfigurable pixelated surface tile 30.
Further details of the component pieces of the present disclosure are described below.
The shape and the inter-pixel gap dimension for the pixels are important design parameters for the RF coupling and/or isolation between pixels 32 and the distributed PCM switch's 34 aspect ratio, which directly translates to the switch's equivalent resistance. Narrower inter-pixel gaps lead to lower required optical actuation power for the PCM switches; however, this may also result in an increase in the RF coupling that may degrade the phased array performance.
An example octagonal patches 32 with spaces 33 between them and PCM switches 34 is shown in
The number of pixels in a tile is determined by the lowest frequency of interest, while the size of the pixel is determined by the tuning resolution needed at the high frequency end.
In one example, a reconfigurable surface tile with a glass substrate 24 with an array of 25×25 pixels, with each patch or pixel 32 1.5 mm square with PCM switches 34 that have a 5 μm width 36 and a 200 μm length 38, could be used to create patch antennas tunable from 2 GHz (S-band) to 12 GHz (X-band). The minimum number of pixels or patches 32 required for this example from 2 GHz (S-band) to 12 GHz (X-band) is shown in the graph of
Note that at f3, as shown in
In
In the configuration of
As discussed above with reference to
The phase change material (PCM) switches 34 have a known property that if the PCM material is heated to one temperature, approximately 300° C. and cooled in a controlled manner, the material will crystallize and become conductive. If the PCM material is heated to a higher temperature, approximately 700° C., and then rapidly quenched it will become amorphous and non-conducting. Thus the switches 34 in the pixelated surface can be actuated and reset by this temperature control. The preferred PCM switch 34 for this present disclosure is fabricated from germanium-telluride (GeTe) doped chalcogenide glass. Chalcogenide glass a glass containing one or more chalcogenide elements. Chalcogenide compounds are widely used in rewritable optical disks and phase-change memory devices and by applying heat, they can be switched between an amorphous and a crystalline state, thereby changing their optical and electrical properties and allowing the storage of information. An application for phase change material is further described in U.S. patent application Ser. No. 13/737,441, filed Jan. 9, 2013, which is incorporated herein as though set forth in full.
The PCM material 34 is fabricated to lie within the gaps of the metallic patches 32 such that when actuated into the on state, the switch 34 would provide a low resistance bridge between two patches, thus effectively connecting them electrically. In this way, actuation of particular patterns of switches 34 by combining various pixels or patches 32 is what creates the reconfigurable planar EM structures such as antennas, transmission lines, or frequency selective surfaces.
An example of how the PCM switches 34 is placed in the gaps between the metallic patches 32 is shown in
The PCM switches 34 can be actuated by placing small heating elements near the switch instead of using optical actuation. However, the bias network for the heating elements would seriously degrade the RF performance of the reconfigurable EM structure. This can be seen in
The optical actuation of this disclosure eliminates the need for bias lines for heater grids. Optical actuation of the PCM switches 34 starts from a corresponding array of focused high power vertical cavity surface emitting lasers (VCSEL) 14, as shown in
In the present disclosure, there is an array of lasers 14 such that each PCM switch 34 is in a one-to-one correspondence with a laser. Vertical cavity surface emitting lasers (VCSELs) 14 are preferred for actuating the switches 34 because they can transmit an optical beam 18, as shown in
The high peak output power of the pulsed multi-mode VCSELs 14 can be used to heat the PCM material segment 34 between each radiating patch 32 of the reconfigurable pixelated surface tile 30 and hence switch its phase and electrical resistance. For GeTe-based PMC material 34, a power density of about 2 mW/μm2 at a pulse width of 700 ns is required to change its initial amorphous phase into polycrystalline, as described in References [5], [6] and [7] below, resulting in more than three orders of magnitude reduction in its electrical resistivity. A power density of about twice this value is required to reverse the PCM 34 to its amorphous phase. These optical power density levels increase as the pulse width is decreased. For example, power densities on the order of 15 to 30 mW/μm2 at 10 to 50 ns pulse widths are currently used for DVD write and erase cycles.
In order to get enough optical power to create a high enough temperature in a given PCM switch 34 to set or reset the switch state, it may be necessary to focus each optical beam 18 to a small spot on that PCM switch 34, which can be performed using a focusing micro-lens array. Multiple VCSELs 14 may be used to actuate a single PCM switch by using multiple multi-mode VCSELs 15 in a linear segment, as shown in
VCSELs 14 are most efficient at wavelengths longer than 950 nm because of the optical gain achievable in the quantum-well structures used. Fortunately, light emitted in the wavelength range of 950 to 980 nm is within the absorption band of the GeTe PCM material, as shown in
In order to concentrate the output power of the multi-mode VCSEL array 14 onto the PCM switch array 34, a set of two custom-designed microlens arrays is placed in between the VCSELs 14 and the reconfigurable pixelated surface tile 30, as shown in
Using the microlens design to focus each 25 μm aperture VCSEL 14 with a peak output power of about 1 W driven at a pulse width of 200 ns or less, may result in an optical power density of more than 50 mW/μm2 incident on the PCM switch 34. This power density level is more than enough to switch the phase of the PMC even at shorter pulse widths. The electrical resistivity of GeTe PCM material is typically about 3×10−6 Ω.m in the polycrystalline phase, and 4 to 5 orders of magnitude higher in its amorphous phase, as described in U.S. patent application Ser. No. 13/737,441, filed Jan. 9, 2013. For a PCM thickness of 500 nm, which is within the absorption depth of 950 nm wavelength light, the electrical resistance of a 5×10 μm2 crystallized segment formed by a focused 25×50 μm2 multi-mode VCSEL element 14 is about 3Ω. Multiple lasers 15, as shown in
The VCSEL arrays 14 used to optically activate the PCM switches 34 in each reconfigurable pixelated surface tile 30 require appropriate control and drive electronic circuitry. An example of a laser driver switch matrix system sufficient to provide current pulse outputs to 1250 VCSELS 14 within 1 milliseconds is shown in
An example of an extension of this approach to a larger tile or to multiple tiles is shown in
References [1]-[7] below are incorporated herein as though set forth in full.
Having now described the present disclosure in accordance with the requirements of the patent statutes, those skilled in this art will understand how to make changes and modifications to the present invention to meet their specific requirements or conditions. Such changes and modifications may be made without departing from the scope and spirit of the present disclosure as disclosed herein.
The foregoing Detailed Description of exemplary and preferred embodiments is presented for purposes of illustration and disclosure in accordance with the requirements of the law. It is not intended to be exhaustive nor to limit the present disclosure to the precise form(s) described, but only to enable others skilled in the art to understand how the present disclosure may be suited for a particular use or implementation. The possibility of modifications and variations will be apparent to practitioners skilled in the art. No limitation is intended by the description of exemplary embodiments which may have included tolerances, feature dimensions, specific operating conditions, engineering specifications, or the like, and which may vary between implementations or with changes to the state of the art, and no limitation should be implied therefrom. Applicant has made this disclosure with respect to the current state of the art, but also contemplates advancements and that adaptations in the future may take into consideration of those advancements, namely in accordance with the then current state of the art. It is intended that the scope of the present disclosure be defined by the Claims as written and equivalents as applicable. Reference to a claim element in the singular is not intended to mean “one and only one” unless explicitly so stated. Moreover, no element, component, nor method or process step in this disclosure is intended to be dedicated to the public regardless of whether the element, component, or step is explicitly recited in the Claims. No claim element herein is to be construed under the provisions of 35 U.S.C. Sec. 112, sixth paragraph, unless the element is expressly recited using the phrase “means for . . . ” and no method or process step herein is to be construed under those provisions unless the step, or steps, are expressly recited using the phrase “comprising the step(s) of . . . . ”
This application is related to U.S. patent application Ser. No. 13/737,441, filed Jan. 9, 2013, and is related to and claims priority to U.S. Provisional Patent Application Ser. No. 61/940,070, filed Feb. 14, 2014, which are incorporated herein as though set forth in full.
This invention was made under U.S. Government contract HR0011-14-0059 Arrays at Commercial Timescales (ACT) issued by DARPA. The U.S. Government has certain rights in this invention.
Number | Date | Country | |
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61940070 | Feb 2014 | US |