EP3800735A1 - Dynamische polarisation und kopplungssteuerung für eine steuerbare zylindrisch gespeiste holografische antenne - Google Patents

Dynamische polarisation und kopplungssteuerung für eine steuerbare zylindrisch gespeiste holografische antenne Download PDF

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Publication number
EP3800735A1
EP3800735A1 EP20210250.5A EP20210250A EP3800735A1 EP 3800735 A1 EP3800735 A1 EP 3800735A1 EP 20210250 A EP20210250 A EP 20210250A EP 3800735 A1 EP3800735 A1 EP 3800735A1
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EP
European Patent Office
Prior art keywords
antenna
layer
feed
slots
wave
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Granted
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EP20210250.5A
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English (en)
French (fr)
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EP3800735B1 (de
Inventor
Adam Bily
Nathan Kundtz
Mikala Johnson
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Kymeta Corp
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Kymeta Corp
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Priority claimed from US14/550,178 external-priority patent/US9887456B2/en
Application filed by Kymeta Corp filed Critical Kymeta Corp
Priority to EP22207471.8A priority Critical patent/EP4191794A1/de
Publication of EP3800735A1 publication Critical patent/EP3800735A1/de
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Publication of EP3800735B1 publication Critical patent/EP3800735B1/de
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/20—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a curvilinear path
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/0006—Particular feeding systems
    • H01Q21/0012—Radial guide fed arrays
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/0006—Particular feeding systems
    • H01Q21/0031—Parallel-plate fed arrays; Lens-fed arrays
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061—Two dimensional planar arrays
    • H01Q21/065—Patch antenna array
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/28—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the amplitude
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • H01Q9/0442—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular tuning means
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04—Resonant antennas
    • H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • H01Q9/045—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular feeding means
    • H01Q9/0457—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular feeding means electromagnetically coupled to the feed line

Definitions

  • Embodiments of the present invention relate to the field of antennas; more particularly, embodiments of the present invention relate to an antenna that is cylindrically fed.
  • VCTS Variable Inclined Transverse Stub
  • Prior approaches use a waveguide and splitter feed structure to feed antennas.
  • the waveguide designs have impedance swing near broadside (a band gap created by 1-wavelength periodic structures); require bonding with unlike CTEs; have an associated ohmic loss of the feed structure; and/or have thousands of vias to extend to the ground-plane.
  • the antenna comprises an antenna feed to input a cylindrical feed wave and a tunable slotted array coupled to the antenna feed.
  • Embodiments of the invention include an antenna design architecture that feeds the antenna from a central point with an excitation (feed wave) that spreads in a cylindrical or concentric manner outward from the feed point.
  • the antenna works by arranging multiple cylindrically fed subaperture antennas (e.g., patch antennas) with the feed wave.
  • the antenna is fed from the perimeter inward, rather than from the center outward. This can be helpful because it counteracts the amplitude excitation decay caused by scattering energy from the aperture. Scattering occurs similarly in both orientations, but the natural taper caused by focusing of the energy in the feed wave as it travels from the perimeter inward counteracts the decreasing taper caused by the intended scattering.
  • Embodiments of the invention include a holographic antenna based on doubling the density typically required to achieve holography and filling the aperture with two types of orthogonal sets of elements.
  • one set of elements is linearly oriented at +45 degrees relative to the feed wave, and the second set of elements is oriented at -45 degrees relative to the feed wave. Both types are illuminated by the same feed wave, which, in one form, is a parallel plate mode launched by a coaxial pin feed.
  • the antenna system is a component or subsystem of a satellite earth station (ES) operating on a mobile platform (e.g., aeronautical, maritime, land, etc.) that operates using either Ka-band frequencies or Ku-band frequencies for civil commercial satellite communications.
  • ES satellite earth station
  • mobile platform e.g., aeronautical, maritime, land, etc.
  • embodiments of the antenna system also can be used in earth stations that are not on mobile platforms (e.g., fixed or transportable earth stations).
  • the antenna system uses surface scattering metamaterial technology to form and steer transmit and receive beams through separate antennas.
  • the antenna systems are analog systems, in contrast to antenna systems that employ digital signal processing to electrically form and steer beams (such as phased array antennas).
  • the antenna system is comprised of three functional subsystems: (1) a wave propagating structure consisting of a cylindrical wave feed architecture; (2) an array of wave scattering metamaterial unit cells; and (3) a control structure to command formation of an adjustable radiation field (beam) from the metamaterial scattering elements using holographic principles.
  • Figure 1 illustrates a top view of one embodiment of a coaxial feed that is used to provide a cylindrical wave feed.
  • the coaxial feed includes a center conductor and an outer conductor.
  • the cylindrical wave feed architecture feeds the antenna from a central point with an excitation that spreads outward in a cylindrical manner from the feed point. That is, a cylindrically fed antenna creates an outward travelling concentric feed wave. Even so, the shape of the cylindrical feed antenna around the cylindrical feed can be circular, square or any shape.
  • a cylindrically fed antenna creates an inward travelling feed wave. In such a case, the feed wave most naturally comes from a circular structure.
  • Figure 2A illustrates a side view of one embodiment of a cylindrically fed antenna structure.
  • the antenna produces an inwardly travelling wave using a double layer feed structure (i.e., two layers of a feed structure).
  • the antenna includes a circular outer shape, though this is not required. That is, non-circular inward travelling structures can be used.
  • the antenna structure in Figure 2A includes the coaxial feed of Figure 1 .
  • a coaxial pin 201 is used to excite the field on the lower level of the antenna.
  • coaxial pin 201 is a 50 ⁇ coax pin that is readily available.
  • Coaxial pin 201 is coupled (e.g., bolted) to the bottom of the antenna structure, which is conducting ground plane 202.
  • interstitial conductor 203 Separate from conducting ground plane 202 is interstitial conductor 203, which is an internal conductor.
  • conducting ground plane 202 and interstitial conductor 203 are parallel to each other.
  • the distance between ground plane 202 and interstitial conductor 203 is 0.1 - 0.15". In another embodiment, this distance may be ⁇ /2, where ⁇ is the wavelength of the travelling wave at the frequency of operation.
  • Ground plane 202 is separated from interstitial conductor 203 via a spacer 204.
  • spacer 204 is a foam or air-like spacer.
  • spacer 204 comprises a plastic spacer.
  • dielectric layer 205 On top of interstitial conductor 203 is dielectric layer 205.
  • dielectric layer 205 is plastic.
  • Figure 5 illustrates an example of a dielectric material into which a feed wave is launched. The purpose of dielectric layer 205 is to slow the travelling wave relative to free space velocity. In one embodiment, dielectric layer 205 slows the travelling wave by 30% relative to free space.
  • the range of indices of refraction that are suitable for beam forming are 1.2 - 1.8, where free space has by definition an index of refraction equal to 1.
  • Other dielectric spacer materials such as, for example, plastic, may be used to achieve this effect. Note that materials other than plastic may be used as long as they achieve the desired wave slowing effect.
  • a material with distributed structures may be used as dielectric 205, such as periodic sub-wavelength metallic structures that can be machined or lithographically defined, for example.
  • An RF-array 206 is on top of dielectric 205.
  • the distance between interstitial conductor 203 and RF-array 206 is 0.1 - 0.15". In another embodiment, this distance may be ⁇ eff /2, where ⁇ eff is the effective wavelength in the medium at the design frequency.
  • the antenna includes sides 207 and 208.
  • Sides 207 and 208 are angled to cause a travelling wave feed from coax pin 201 to be propagated from the area below interstitial conductor 203 (the spacer layer) to the area above interstitial conductor 203 (the dielectric layer) via reflection.
  • the angle of sides 207 and 208 are at 45° angles.
  • sides 207 and 208 could be replaced with a continuous radius to achieve the reflection. While Figure 2A shows angled sides that have angle of 45 degrees, other angles that accomplish signal transmission from lower level feed to upper level feed may be used.
  • the 45° angles are replaced with a single step such as shown in Figure 20 .
  • steps 2001 and 2002 are shown on one end of the antenna around dielectric layer 2005, interstitial conductor 2003, and spacer layer 2004. The same two steps are at the other ends of these layers.
  • the wave In operation, when a feed wave is fed in from coaxial pin 201, the wave travels outward concentrically oriented from coaxial pin 201 in the area between ground plane 202 and interstitial conductor 203.
  • the concentrically outgoing waves are reflected by sides 207 and 208 and travel inwardly in the area between interstitial conductor 203 and RF array 206.
  • the reflection from the edge of the circular perimeter causes the wave to remain in phase (i.e., it is an in-phase reflection).
  • the travelling wave is slowed by dielectric layer 205. At this point, the travelling wave starts interacting and exciting with elements in RF array 206 to obtain the desired scattering.
  • termination 209 is included in the antenna at the geometric center of the antenna.
  • termination 209 comprises a pin termination (e.g., a 50 ⁇ pin).
  • termination 209 comprises an RF absorber that terminates unused energy to prevent reflections of that unused energy back through the feed structure of the antenna. These could be used at the top of RF array 206.
  • FIG. 2B illustrates another embodiment of the antenna system with an outgoing wave.
  • two ground planes 210 and 211 are substantially parallel to each other with a dielectric layer 212 (e.g., a plastic layer, etc.) in between ground planes 210 and 211.
  • RF absorbers 213 and 214 e.g., resistors
  • a coaxial pin 215 e.g., 50 ⁇
  • An RF array 216 is on top of dielectric layer 212.
  • a feed wave is fed through coaxial pin 215 and travels concentrically outward and interacts with the elements of RF array 216.
  • the cylindrical feed in both the antennas of Figures 2A and 2B improves the service angle of the antenna.
  • the antenna system has a service angle of seventy five degrees (75°) from the bore sight in all directions.
  • the overall antenna gain is dependent on the gain of the constituent elements, which themselves are angle-dependent.
  • the overall antenna gain typically decreases as the beam is pointed further off bore sight. At 75 degrees off bore sight, significant gain degradation of about 6 dB is expected.
  • Embodiments of the antenna having a cylindrical feed solve one or more problems. These include dramatically simplifying the feed structure compared to antennas fed with a corporate divider network and therefore reducing total required antenna and antenna feed volume; decreasing sensitivity to manufacturing and control errors by maintaining high beam performance with coarser controls (extending all the way to simple binary control); giving a more advantageous side lobe pattern compared to rectilinear feeds because the cylindrically oriented feed waves result in spatially diverse side lobes in the far field; and allowing polarization to be dynamic, including allowing left-hand circular, right-hand circular, and linear polarizations, while not requiring a polarizer.
  • RF array 206 of Figure 2A and RF array 216 of Figure 2B include a wave scattering subsystem that includes a group of patch antennas (i.e., scatterers) that act as radiators.
  • This group of patch antennas comprises an array of scattering metamaterial elements.
  • each scattering element in the antenna system is part of a unit cell that consists of a lower conductor, a dielectric substrate and an upper conductor that embeds a complementary electric inductive-capacitive resonator ("complementary electric LC" or “CELC”) that is etched in or deposited onto the upper conductor.
  • a complementary electric inductive-capacitive resonator (“complementary electric LC” or “CELC”) that is etched in or deposited onto the upper conductor.
  • a liquid crystal is injected in the gap around the scattering element.
  • Liquid crystal is encapsulated in each unit cell and separates the lower conductor associated with a slot from an upper conductor associated with its patch.
  • Liquid crystal has a permittivity that is a function of the orientation of the molecules comprising the liquid crystal, and the orientation of the molecules (and thus the permittivity) can be controlled by adjusting the bias voltage across the liquid crystal. Using this property, the liquid crystal acts as an on/off switch for the transmission of energy from the guided wave to the CELC. When switched on, the CELC emits an electromagnetic wave like an electrically small dipole antenna.
  • Controlling the thickness of the LC increases the beam switching speed.
  • a fifty percent (50%) reduction in the gap between the lower and the upper conductor results in a fourfold increase in speed.
  • the thickness of the liquid crystal results in a beam switching speed of approximately fourteen milliseconds (14 ms).
  • the LC is doped in a manner well-known in the art to improve responsiveness so that a seven millisecond (7 ms) requirement can be met.
  • the CELC element is responsive to a magnetic field that is applied parallel to the plane of the CELC element and perpendicular to the CELC gap complement.
  • a voltage is applied to the liquid crystal in the metamaterial scattering unit cell, the magnetic field component of the guided wave induces a magnetic excitation of the CELC, which, in turn, produces an electromagnetic wave in the same frequency as the guided wave.
  • the phase of the electromagnetic wave generated by a single CELC can be selected by the position of the CELC on the vector of the guided wave.
  • Each cell generates a wave in phase with the guided wave parallel to the CELC. Because the CELCs are smaller than the wave length, the output wave has the same phase as the phase of the guided wave as it passes beneath the CELC.
  • the cylindrical feed geometry of this antenna system allows the CELC elements to be positioned at forty five degree (45°) angles to the vector of the wave in the wave feed. This position of the elements enables control of the polarization of the free space wave generated from or received by the elements.
  • the CELCs are arranged with an inter-element spacing that is less than a free-space wavelength of the operating frequency of the antenna. For example, if there are four scattering elements per wavelength, the elements in the 30 GHz transmit antenna will be approximately 2.5 mm (i.e., 1/4th the 10 mm free-space wavelength of 30 GHz).
  • the CELCs are implemented with patch antennas that include a patch co-located over a slot with liquid crystal between the two.
  • the metamaterial antenna acts like a slotted (scattering) wave guide. With a slotted wave guide, the phase of the output wave depends on the location of the slot in relation to the guided wave.
  • FIG 3 illustrates a top view of one embodiment of one patch antenna, or scattering element.
  • the patch antenna comprises a patch 301 collocated over a slot 302 with liquid crystal (LC) 303 in between patch 301 and slot 302.
  • LC liquid crystal
  • FIG 4 illustrates a side view of a patch antenna that is part of a cyclically fed antenna system.
  • the patch antenna is above dielectric 402 (e.g., a plastic insert, etc.) that is above the interstitial conductor 203 of Figure 2A (or a ground conductor such as in the case of the antenna in Figure 2B ).
  • dielectric 402 e.g., a plastic insert, etc.
  • An iris board 403 is a ground plane (conductor) with a number of slots, such as slot 403a on top of and over dielectric 402.
  • a slot may be referred to herein as an iris.
  • the slots in iris board 403 are created by etching. Note that in one embodiment, the highest density of slots, or the cells of which they are a part, is ⁇ /2. In one embodiment, the density of slots/cells is ⁇ /3 (i.e., 3 cells per ⁇ ). Note that other densities of cells may be used.
  • a patch board 405 containing a number of patches, such as patch 405a, is located over the iris board 403, separated by an intermediate dielectric layer.
  • Each of the patches, such as patch 405a, are co-located with one of the slots in iris board 403.
  • the intermediate dielectric layer between iris board 403 and patch board 405 is a liquid crystal substrate layer 404.
  • the liquid crystal acts as a dielectric layer between each patch and its co-located slot. Note that substrate layers other than LC may be used.
  • patch board 405 comprises a printed circuit board (PCB), and each patch comprises metal on the PCB, where the metal around the patch has been removed.
  • PCB printed circuit board
  • patch board 405 includes vias for each patch that is on the side of the patch board opposite the side where the patch faces its co-located slot.
  • the vias are used to connect one or more traces to a patch to provide voltage to the patch.
  • matrix drive is used to apply voltage to the patches to control them. The voltage is used to tune or detune individual elements to effectuate beam forming.
  • the patches may be deposited on the glass layer (e.g., a glass typically used for LC displays (LCDs) such as, for example, Corning Eagle glass), instead of using a circuit patch board.
  • FIG 17 illustrates a portion of a cylindrically fed antenna that includes a glass layer that contains the patches.
  • the antenna includes conductive base or ground layer 1701, dielectric layer 1702 (e.g., plastic), iris board 1703 (e.g., a circuit board) containing slots, a liquid crystal substrate layer 1704, and a glass layer 1705 containing patches 1710.
  • the patches 1710 have a rectangular shape.
  • the slots and patches are positioned in rows and columns, and the orientation of patches is the same for each row or column while the orientation of the co-located slots are oriented the same with respect to each other for rows or columns, respectively.
  • a cap e.g., a radome cap covers the top of the patch antenna stack to provide protection.
  • Figure 6 illustrates one embodiment of iris board 403. This is a lower conductor of the CELCs.
  • the iris board includes an array of slots.
  • each slot is oriented either +45 or -45 relative to the impinging feed wave at the slot's central location.
  • the layout pattern of the scattering elements (CELCs) are arranged at ⁇ 45 degrees to the vector of the wave.
  • a circular opening 403b which is essentially another slot.
  • the slot is on the top of the Iris board and the circular or elliptical opening is on the bottom of the Iris board. Note that these openings, which may be about 0.001" or 25 mm in depth, are optional.
  • the slotted array is tunably directionally loaded. By turning individual slots off or on, each slot is tuned to provide the desired scattering at the operating frequency of the antenna (i.e., it is tuned to operate at a given frequency).
  • Figure 7 illustrates the manner in which the orientation of one iris (slot)/patch combination is determined.
  • the letter A denotes a solid black arrow denoting power feed vector from a cylindrical feed location to the center of an element.
  • the letter B denotes dashed orthogonal lines showing perpendicular axes relative to "A”
  • the letter C denotes a dashed rectangle encircling slot rotated 45 degrees relative to "B”.
  • Figure 8 illustrates irises (slots) grouped into two sets, with the first set rotated at -45 degrees relative to the power feed vector and the second set rotated +45 degrees relative to the power feed vector.
  • group A includes slots whose rotation relative to a feed vector is equal to -45°
  • group B includes slots whose rotation relative to a feed vector is +45°.
  • Figure 9 illustrates an embodiment of patch board 405.
  • the patch board includes rectangular patches covering slots and completing linearly polarized patch/slot resonant pairs to be turned off and on.
  • the pairs are turned off or on by applying a voltage to the patch using a controller.
  • the voltage required is dependent on the liquid crystal mixture being used, the resulting threshold voltage required to begin to tune the liquid crystal, and the maximum saturation voltage (beyond which no higher voltage produces any effect except to eventually degrade or short circuit through the liquid crystal).
  • matrix drive is used to apply voltage to the patches in order to control the coupling.
  • the control structure has 2 main components; the controller, which includes drive electronics, for the antenna system, is below the wave scattering structure, while the matrix drive switching array is interspersed throughout the radiating RF array in such a way as to not interfere with the radiation.
  • the drive electronics for the antenna system comprise commercial off-the shelf LCD controls used in commercial television appliances that adjust the bias voltage for each scattering element by adjusting the amplitude of an AC bias signal to that element.
  • the controller controls the electronics using software controls.
  • the control of the polarization is part of the software control of the antenna and the polarization is pre-programmed to match the polarization of the signal coming from the satellite service with which the earth station is communicating or be pre-programmed to match the polarization of the receiving antenna on the satellite.
  • the controller also contains a microprocessor executing the software.
  • the control structure may also incorporate sensors (nominally including a GPS receiver, a three axis compass and an accelerometer) to provide location and orientation information to the processor.
  • the location and orientation information may be provided to the processor by other systems in the earth station and/or may not be part of the antenna system.
  • the controller controls which elements are turned off and those elements turned on at the frequency of operation.
  • the elements are selectively detuned for frequency operation by voltage application.
  • a controller supplies an array of voltage signals to the RF radiating patches to create a modulation, or control pattern.
  • the control pattern causes the elements to be turned on or off.
  • the control pattern resembles a square wave in which elements along one spiral (LHCP or RHCP) are "on” and those elements away from the spiral are "off' (i.e., a binary modulation pattern).
  • multistate control in which various elements are turned on and off to varying levels, further approximating a sinusoidal control pattern, as opposed to a square wave (i.e., a sinusoid gray shade modulation pattern). Some elements radiate more strongly than others, rather than some elements radiate and some do not. Variable radiation is achieved by applying specific voltage levels, which adjusts the liquid crystal permittivity to varying amounts, thereby detuning elements variably and causing some elements to radiate more than others.
  • the generation of a focused beam by the metamaterial array of elements can be explained by the phenomenon of constructive and destructive interference.
  • Individual electromagnetic waves sum up (constructive interference) if they have the same phase when they meet in free space and waves cancel each other (destructive interference) if they are in opposite phase when they meet in free space.
  • the slots in a slotted antenna are positioned so that each successive slot is positioned at a different distance from the excitation point of the guided wave, the scattered wave from that element will have a different phase than the scattered wave of the previous slot. If the slots are spaced one quarter of a guided wavelength apart, each slot will scatter a wave with a one fourth phase delay from the previous slot.
  • the number of patterns of constructive and destructive interference that can be produced can be increased so that beams can be pointed theoretically in any direction plus or minus ninety degrees (90°) from the bore sight of the antenna array, using the principles of holography.
  • the antenna can change the direction of the wave front.
  • the time required to turn the unit cells on and off dictates the speed at which the beam can be switched from one location to another location.
  • the polarization and beam pointing angle are both defined by the modulation, or control pattern specifying which elements are on or off. In other words, the frequency at which to point the beam and polarize it in the desired way are dependent upon the control pattern. Since the control pattern is programmable, the polarization can be programmed for the antenna system.
  • the desired polarization states are circular or linear for most applications.
  • the circular polarization states include spiral polarization states, namely right-hand circular polarization and left-hand circular polarization, which are shown in Figures 16A and 16B , respectively, for a feed wave fed from the center and travelling outwardly.
  • the orientation, or sense, or the spiral modulation pattern is reversed.
  • the direction of the feed wave i.e. center or edge fed
  • the direction of the feed wave is also specified when stating that a given spiral pattern of on and off elements to result in left-hand or right-hand circular polarization.
  • the control pattern for each beam will be stored in the controller or calculated on the fly, or some combination thereof.
  • the antenna control system determines where the antenna is located and where it is pointing, it then determines where the target satellite is located in reference to the bore sight of the antenna.
  • the controller then commands an on and off pattern of the individual unit cells in the array that corresponds with the preselected beam pattern for the position of the satellite in the field of vision of the antenna.
  • the antenna system produces one steerable beam for the uplink antenna and one steerable beam for the downlink antenna.
  • Figure 10 illustrates an example of elements with patches in Figure 9 that are determined to be off at frequency of operation
  • Figure 11 illustrates an example of elements with patches in Figure 9 that are determined to be on at frequency of operation
  • Figure 12 illustrates the results of full wave modeling that show an electric field response to the on and off modulation pattern with respect to the elements of Figures 10 and 11 .
  • Figure 13 illustrates beam forming.
  • the interference pattern may be adjusted to provide arbitrary antenna radiation patterns by identifying an interference pattern corresponding to a selected beam pattern and then adjusting the voltage across the scattering elements to produce a beam according the principles of holography.
  • the basic principle of holography including the terms "object beam” and “reference beam”, as commonly used in connection with these principles, is well-known.
  • RF holography in the context of forming a desired "object beam” using a traveling wave as a "reference beam” is performed as follows.
  • the modulation pattern is determined as follows. First, a reference wave (beam), sometimes called the feed wave, is generated.
  • Figure 19A illustrates an example of a reference wave. Referring to Figure 19A , rings 1900 are the phase fronts of the electric and magnetic fields of a reference wave. They exhibit sinusoidal time variation. Arrow 1901 illustrates the outward propagation of the reference wave.
  • a TEM, or Transverse Electro-Magnetic, wave travels either inward or outward.
  • the direction of propagation is also defined and for this example outward propagation from a center feed point is chosen.
  • the plane of propagation is along the antenna surface.
  • An object wave sometimes called the object beam
  • the object wave is a TEM wave travelling in direction 30 degrees off normal to the antenna surface, with azimuth set to 0 deg.
  • the polarization is also defined and for this example right handed circular polarization is chosen.
  • the resulting modulation pattern is also a sinusoid.
  • the maxima of the reference wave meets the maxima of the object wave (both sinusoidally time-varying quantities)
  • the modulation pattern is a maxima, or a strongly radiating site.
  • this interference is calculated at each scattering location and is dependent on not just the position, but also the polarization of the element based on its rotation and the polarization of the object wave at the location of the element.
  • Figure 19C is an example of the resulting sinusoidal modulation pattern.
  • the voltage across the scattering elements is controlled by adjusting the voltage applied between the patches and the ground plane, which in this context is the metallization on the top of the iris board.
  • the patches and slots are positioned in a honeycomb pattern. Examples of such a pattern are shown in Figures 14A and 14B .
  • honeycomb structures are such that every other row is shifted left or right by one half element spacing or, alternatively, every other column is shifted up or down by one half the element spacing.
  • the patches and associated slots are positioned in rings to create a radial layout.
  • the slot center is positioned on the rings.
  • Figure 15A illustrates an example of patches (and their co-located slots) being positioned in rings. Referring to Figure 15A , the centers of the patches and slots are on the rings and the rings are concentrically located relative to the feed or termination point of the antenna array. Note that adjacent slots located in the same ring are oriented almost 90° with respect to each other (when evaluated at their center). More specifically, they are oriented at an angle equal to 90° plus the angular displacement along the ring containing the geometric centers of the 2 elements.
  • Figure 15B is an example of a control pattern for a ring based slotted array, such as depicted in Figure 15A .
  • the resulting near fields and far fields for a 30° beam pointing with LHCP are shown in Figure15C , respectively.
  • the feed structure is shaped to control coupling to ensure the power being radiated or scattered is roughly constant across the full 2D aperture. This is accomplished by using a linear thickness taper in the dielectric, or analogous taper in the case of a ridged feed network, that causes less coupling near the feed point and more coupling away from the feed point.
  • the use of a linear taper to the height of the feed counteracts the 1/r decay in the travelling wave as it propagates away from the feed point by containing the energy in a smaller volume, which results in a greater percentage of the remaining energy in the feed scattering from each element. This is important in creating a uniform amplitude excitation across the aperture.
  • this tapering can be applied in a non-radially symmetric manner to cause the power scattered to be roughly constant across the aperture.
  • a complementary technique requires elements to be tuned differently in the array based on how far they are from the feed point.
  • One example of a taper is implemented using a dielectric in a Maxwell fish-eye lens shape producing an inversely proportional increase in radiation intensity to counteract the 1/r decay.
  • Figure 18 illustrates a linear taper of a dielectric.
  • a tapered dielectric 1802 is shown having a coaxial feed 1800 to provide a concentric feed wave to execute elements (patch/iris pairs) of RF array 1801.
  • Dielectric 1802 e.g., plastic
  • height B is greater than the height A as it is closer to coaxial feed 1800.
  • dielectrics are formed with a non-radially symmetric shape to focus energy where needed.
  • the path length from the center to a corner of a square is 1.4 times longer than from the center to the center of a side of a square. Therefore, more energy must be focused toward the 4 corners than toward the 4 halfway points of the sides of the square, and the rate of energy scattering must also be different.
  • Non-radially symmetric shaping of the feed and other structures can accomplish these requirements
  • dissimilar dielectrics are stacked in a given feed structure to control power scattering from feed to aperture as wave radiates outward.
  • the electric or magnetic energy intensity can be concentrated in a particular dielectric medium when more than 1 dissimilar dielectric media are stacked on top of each other.
  • One specific example is using a plastic layer and an air-like foam layer whose total thickness is less than ⁇ eff /2 at the operation frequency, which results in higher concentration of magnetic field energy in the plastic than the air-like foam.
  • control pattern is controlled spatially (turning on fewer elements at the beginning, for instance) for patch/iris detuning to control coupling over the aperture and to scatter more or less energy depending on direction of feeding and desired aperture excitation weighting.
  • the control pattern used at the beginning turns on fewer slots than the rest of the time. For instance, at the beginning, only a certain percentage of the elements (e.g., 40%, 50%) (patch/iris slot pairs) near the center of the cylindrical feed that are going to be turned on to form a beam are turned on during a first stage and then the remaining are turned that are further out from the cylindrical feed.
  • elements could be turned on continuously from the cylindrical feed as the wave propagates away from the feed.
  • a ridged feed network replaces the dielectric spacer (e.g., the plastic of spacer 205) and allows further control of the orientation of propagating feed wave.
  • Ridges can be used to create asymmetric propagation in the feed (i.e., the Poynting vector is not parallel to the wave vector) to counteract the 1/r decay.
  • the use of ridges within the feed helps direct energy where needed. By directing more ridges and/or variable height ridges to low energy areas, a more uniform illumination is created at the aperture. This allows a deviation from a purely radial feed configuration because the direction of propagation of the feed wave may no longer be oriented radially. Slots over a ridge couple strongly, while those slots between the ridges couple weakly. Thus, depending on the desired coupling (to obtain the desired beam), the use of ridge and the placement of slots allows control of coupling.
  • a complex feed structure that provides an aperture illumination that is not circularly symmetric is used.
  • Such an application could be a square or generally non-circular aperture which is illuminated non-uniformly.
  • a non-radially symmetric dielectric that delivers more energy to some regions than to others is used. That is, the dielectric can have areas with different dielectric controls.
  • a dielectric distribution that looks like a Maxwell fish-eye lens. This lens would deliver different amounts of power to different parts of the array.
  • a ridged feed structure is used to deliver more energy to some regions than to others.
  • multiple cylindrically-fed sub-aperture antennas of the type described here are arrayed.
  • one or more additional feed structures are used.
  • distributed amplification points are included.
  • an antenna system may include multiple antennas such as those shown in Figure 2A or 2B in an array.
  • the array system may be 3x3 (9 total antennas), 4x4, 5x5, etc., but other configurations are possible.
  • each antenna may have a separate feed.
  • the number of amplification points may be less than the number of feeds.
  • One advantage to embodiments of the present invention architecture is better beam performance than linear feeds.
  • the natural, built-in taper at the edges can help to achieve good beam performance.
  • the FCC mask can be met from a 40cm aperture with only on and off elements.
  • embodiments of the invention have no impedance swing near broadside, no band-gap created by 1-wavelength periodic structures.
  • Embodiments of the invention have no diffractive mode problems when scanning off broadside.
  • On-off modes of operation have opportunities for extended dynamic and instantaneous bandwidths because the mode of operation does not require each element to be tuned to a particular portion of its resonance curve.
  • the antenna can operate continuously through both amplitude and phase hologram portions of its range without significant performance impact. This places the operational range much closer to total tunable range.
  • the cylindrical feed structure can take advantage of a TFT architecture, which implies functioning on quartz or glass. These substrates are much harder than circuit boards, and there are better known techniques for achieving gap sizes around 3um. A gap size of 3um would result in a 14ms switching speed.
  • Disclosed architectures described herein require no machining work and only a single bond stage in production. This, combined with the switch to TFT drive electronics, eliminates costly materials and some tough requirements.
  • Example 1 is an antenna comprising: an antenna feed to input a cylindrical feed wave; and a tunable slotted array coupled to the antenna feed.
  • Example 2 is an antenna as indicated in Example 1 wherein the slotted array is dielectrically loaded.
  • Example 3 is an antenna as indicated in Example 1 wherein the slotted array comprises a plurality of slots and further wherein each slot is tuned to provide a desired scattering at a given frequency.
  • Example 4 is an antenna as indicated in Example 3 wherein each slot of the plurality of slots is oriented either +45 degrees or -45 degrees relative to the cylindrical feed wave impinging at a central location of said each slot, such that the slotted array includes a first set of slots rotated +45 degrees relative to the cylindrical feed wave propagation direction and a second set of slots rotated -45 degrees relative to the propagation direction of the cylindrical feed wave.
  • Example 5 is an antenna as indicated in Example 1 wherein the slotted array comprises:
  • Example 6 is an antenna as indicated in Example 5 wherein a dielectric is between each slot of the plurality of slots and its associated patch in the plurality of patches.
  • Example 7 is an antenna as indicated in Example 6 wherein the dielectric comprises liquid crystal.
  • Example 8 is an antenna as indicated in Example 6 further comprising a controller that applies a control pattern that controls which patch/slot pairs are on and off, thereby causing generation of a beam.
  • Example 9 is an antenna as indicated in Example 8 wherein the control pattern turns on only a subset of the patch/slot pairs that are used to generate the beam during a first stage and then turns on the remaining patch/slot pairs that are used to generate the beam during a second stage.
  • Example 10 is an antenna as indicated in Example 5 wherein the plurality of patches are positioned in a plurality of rings, the plurality of rings are concentrically located relative to the antenna feed of the slotted array.
  • Example 11 is an antenna as indicated in Example 5 wherein the plurality of patches is included in a patch board.
  • Example 12 is an antenna as indicated in Example 5 wherein the plurality of patches are included in a glass layer.
  • Example 13 is an antenna as indicated in Example 1 further comprising a dielectric layer into which the cylindrical feed wave travels.
  • Example 14 is an antenna d as indicated in Example 13 further comprising:
  • Example 15 is an antenna as indicated in Example 14 further comprising at least one RF absorber coupled to the ground plane and the slotted array to terminate unused energy to prevent reflections of that the unused energy back through the antenna.
  • Example 16 is an antenna as indicated in Example 14 further comprising:
  • Example 17 is an antenna as indicated in Example 16 wherein the side area comprises two sides, each of the two side areas angled to cause the feed wave to propagate from the spacer layer of the feed to the dielectric layer of the feed.
  • Example 18 is an antenna as indicated in Example 16 wherein the spacer comprises foam.
  • Example 19 is an antenna as indicated in Example 13 wherein the dielectric layer comprises plastic.
  • Example 20 is an antenna as indicated in Example 13 wherein the dielectric layer is tapered.
  • Example 21 is an antenna as indicated in Example 13 wherein the dielectric layer includes a plurality of areas that have different dielectric constants.
  • Example 22 is an antenna as indicated in Example 13 wherein the dielectric layer includes a plurality of distributed structures that affects propagation of the feed wave.
  • Example 23 is an antenna as indicated in Example 1 further comprising a ridged feed network into which the cylindrical feed wave travels.
  • Example 24 is an antenna comprising: an antenna feed to input a feed wave that propagates concentrically from the feed; a dielectric layer through which the feed wave travels; a plurality of slots; a plurality of patches, wherein each of the patches is co-located over and separated from a slot in the plurality of slots using a liquid crystal layer and forming a patch/slot pair, each patch/slot pair being turned off or on based on application of a voltage to the patch in the pair specified by a control pattern.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)
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US14/550,178 US9887456B2 (en) 2014-02-19 2014-11-21 Dynamic polarization and coupling control from a steerable cylindrically fed holographic antenna
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Families Citing this family (79)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108140945B (zh) 2015-10-09 2020-07-07 夏普株式会社 扫描天线及其驱动方法
WO2017061527A1 (ja) 2015-10-09 2017-04-13 シャープ株式会社 Ｔｆｔ基板、それを用いた走査アンテナ、およびｔｆｔ基板の製造方法
JP6139044B1 (ja) 2015-10-15 2017-05-31 シャープ株式会社 走査アンテナおよびその製造方法
US10777887B2 (en) 2015-10-15 2020-09-15 Sharp Kabushiki Kaisha Scanning antenna and method for manufacturing same
CN108140946B (zh) 2015-10-15 2020-08-25 夏普株式会社 扫描天线及其制造方法
CN108432047B (zh) 2015-12-28 2020-11-10 夏普株式会社 扫描天线及其制造方法
CN107408759B (zh) 2016-01-29 2018-11-09 夏普株式会社 扫描天线
US10498019B2 (en) 2016-01-29 2019-12-03 Sharp Kabushiki Kaisha Scanning antenna
JP6554224B2 (ja) 2016-02-16 2019-07-31 シャープ株式会社 走査アンテナ
WO2017142032A1 (ja) 2016-02-19 2017-08-24 シャープ株式会社 走査アンテナおよびその製造方法
CN108780946B (zh) 2016-03-11 2021-01-15 夏普株式会社 扫描天线及扫描天线的检查方法
US10637141B2 (en) 2016-03-29 2020-04-28 Sharp Kabushiki Kaisha Scanning antenna, method for inspecting scanning antenna, and method for manufacturing scanning antenna
US10763583B2 (en) 2016-05-10 2020-09-01 Kymeta Corporation Method to assemble aperture segments of a cylindrical feed antenna
WO2017199777A1 (ja) 2016-05-16 2017-11-23 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
WO2017204114A1 (ja) 2016-05-27 2017-11-30 シャープ株式会社 走査アンテナおよび走査アンテナの製造方法
CN109314316B (zh) 2016-05-30 2020-10-23 夏普株式会社 扫描天线
CN109314145B (zh) 2016-06-09 2021-07-13 夏普株式会社 Tft基板、具备tft基板的扫描天线、以及tft基板的制造方法
WO2017213148A1 (ja) 2016-06-10 2017-12-14 シャープ株式会社 走査アンテナ
CN109564944B (zh) * 2016-07-19 2021-12-28 夏普株式会社 Tft基板、具备tft基板的扫描天线、以及tft基板的制造方法
JP6691213B2 (ja) 2016-07-26 2020-04-28 シャープ株式会社 走査アンテナおよび走査アンテナの製造方法
WO2018021154A1 (ja) 2016-07-27 2018-02-01 シャープ株式会社 走査アンテナおよび走査アンテナの駆動方法ならびに液晶デバイス
WO2018021310A1 (ja) 2016-07-28 2018-02-01 シャープ株式会社 走査アンテナ
WO2018030180A1 (ja) 2016-08-08 2018-02-15 シャープ株式会社 走査アンテナ
CN109643848B (zh) 2016-08-12 2021-04-13 夏普株式会社 扫描天线
CN109565115B (zh) * 2016-08-17 2021-03-09 夏普株式会社 扫描天线用液晶单元及扫描天线用液晶单元的制造方法
CN109643849B (zh) 2016-08-26 2021-03-09 夏普株式会社 扫描天线
US11189914B2 (en) * 2016-09-26 2021-11-30 Sharp Kabushiki Kaisha Liquid crystal cell and scanning antenna
CN109844626A (zh) * 2016-10-06 2019-06-04 夏普株式会社 液晶单元的制造方法和液晶单元
US10790319B2 (en) 2016-10-27 2020-09-29 Sharp Kabushiki Kaisha TFT substrate, scanning antenna provided with TFT substrate and method for producing TFT substrate
JP6717970B2 (ja) 2016-11-09 2020-07-08 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
US11041891B2 (en) 2016-11-29 2021-06-22 Sharp Kabushiki Kaisha Liquid crystal device, method for measuring residual DC voltage in liquid crystal device, method for driving liquid crystal device, and method for manufacturing liquid crystal device
WO2018105520A1 (ja) * 2016-12-08 2018-06-14 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
CN110050351B (zh) * 2016-12-09 2022-06-10 夏普株式会社 Tft基板、具备tft基板的扫描天线以及tft基板的制造方法
US11049658B2 (en) * 2016-12-22 2021-06-29 Kymeta Corporation Storage capacitor for use in an antenna aperture
WO2018123696A1 (ja) * 2016-12-28 2018-07-05 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
CN110192306B (zh) 2017-01-13 2021-02-05 夏普株式会社 扫描天线和扫描天线的制造方法
KR20180096280A (ko) * 2017-02-21 2018-08-29 삼성전자주식회사 안테나 장치 및 이를 포함하는 전자 장치
CN110326114B (zh) * 2017-02-28 2022-04-22 夏普株式会社 Tft基板、具备tft基板的扫描天线以及tft基板的制造方法
CN110392930B (zh) * 2017-03-03 2023-06-30 夏普株式会社 Tft基板和具备tft基板的扫描天线
CN110446970B (zh) 2017-03-23 2022-07-05 夏普株式会社 液晶单位以及扫描天线
CN110476113B (zh) 2017-03-30 2022-08-16 夏普株式会社 液晶单元和扫描天线
CN110462843B (zh) 2017-04-06 2023-07-07 夏普株式会社 Tft基板和具备tft基板的扫描天线
WO2018186309A1 (ja) 2017-04-07 2018-10-11 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
CN110462842B (zh) 2017-04-07 2022-05-17 夏普株式会社 Tft基板、具备tft基板的扫描天线以及tft基板的制造方法
CN107275805B (zh) * 2017-04-27 2018-08-03 北京华镁钛科技有限公司 一种基于超材料电磁特性的相控阵天线
CN108879112B (zh) * 2017-05-12 2021-02-09 华为技术有限公司 天线阵列及终端
WO2018221327A1 (ja) 2017-05-31 2018-12-06 シャープ株式会社 Ｔｆｔ基板およびｔｆｔ基板を備えた走査アンテナ
CN110770882B (zh) 2017-06-15 2023-12-01 夏普株式会社 Tft基板和具备tft基板的扫描天线
CN109119756B (zh) * 2017-06-22 2020-06-23 北京机电工程研究所 一种大角度扫描微带相控阵天线
US10811769B2 (en) * 2017-06-30 2020-10-20 Innolux Corporation Liquid-crystal antenna apparatus and method for tracking wireless apparatus using the same
CN109216887A (zh) * 2017-06-30 2019-01-15 群创光电股份有限公司 液晶天线装置
US11387260B2 (en) 2017-07-12 2022-07-12 Sharp Kabushiki Kaisha TFT substrate, scanning antenna provided with TFT substrate, and manufacturing method of TFT substrate
WO2019031392A1 (ja) 2017-08-09 2019-02-14 シャープ株式会社 走査アンテナおよび走査アンテナの製造方法
WO2019031395A1 (ja) 2017-08-10 2019-02-14 シャープ株式会社 Ｔｆｔモジュール、ｔｆｔモジュールを備えた走査アンテナ、ｔｆｔモジュールを備えた装置の駆動方法、およびｔｆｔモジュールを備えた装置の製造方法
JP2019062090A (ja) 2017-09-27 2019-04-18 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
JP6578334B2 (ja) 2017-09-27 2019-09-18 シャープ株式会社 Ｔｆｔ基板およびｔｆｔ基板を備えた走査アンテナ
JP2019087852A (ja) 2017-11-06 2019-06-06 シャープ株式会社 走査アンテナおよび液晶装置
JP2019091835A (ja) 2017-11-16 2019-06-13 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
JP2019125908A (ja) 2018-01-16 2019-07-25 シャープ株式会社 液晶セル、及び走査アンテナ
JP2019128541A (ja) 2018-01-26 2019-08-01 シャープ株式会社 液晶セル、及び走査アンテナ
JP2019134032A (ja) 2018-01-30 2019-08-08 シャープ株式会社 Ｔｆｔ基板、ｔｆｔ基板を備えた走査アンテナ、およびｔｆｔ基板の製造方法
US11139695B2 (en) 2018-02-12 2021-10-05 Ossia Inc. Flat panel substrate with integrated antennas and wireless power transmission system
WO2019181706A1 (ja) 2018-03-20 2019-09-26 Ａｇｃ株式会社 基板、液晶アンテナ及び高周波デバイス
KR20200133340A (ko) 2018-03-20 2020-11-27 에이지씨 가부시키가이샤 유리 기판, 액정 안테나 및 고주파 디바이스
CN109088177B (zh) * 2018-08-07 2021-07-02 江西师范大学 双圆极化波导阵列天线及其制作方法
JP2020053759A (ja) 2018-09-25 2020-04-02 シャープ株式会社 走査アンテナおよびｔｆｔ基板
JP7055900B2 (ja) 2018-12-12 2022-04-18 シャープ株式会社 走査アンテナおよび走査アンテナの製造方法
JP7027571B2 (ja) 2018-12-12 2022-03-01 シャープ株式会社 走査アンテナおよび走査アンテナの製造方法
US11616305B2 (en) 2018-12-12 2023-03-28 Sharp Kabushiki Kaisha Scanning antenna and method for manufacturing scanning antenna
US11217611B2 (en) 2019-04-09 2022-01-04 Sharp Kabushiki Kaisha Scanned antenna and method for manufacturing same
US11258176B2 (en) * 2019-04-12 2022-02-22 Kymeta Corporation Non-circular center-fed antenna and method for using the same
US11502408B2 (en) 2019-04-25 2022-11-15 Sharp Kabushiki Kaisha Scanned antenna and liquid crystal device
US11431106B2 (en) 2019-06-04 2022-08-30 Sharp Kabushiki Kaisha TFT substrate, method for manufacturing TFT substrate, and scanned antenna
WO2021000137A1 (zh) * 2019-06-30 2021-01-07 瑞声声学科技(深圳)有限公司 天线振子
CN111146572B (zh) * 2019-12-20 2021-12-24 中国电波传播研究所（中国电子科技集团公司第二十二研究所） 一种折合式圆极化反射阵天线
US11837785B2 (en) 2020-08-04 2023-12-05 Sony Group Corporation Holographic antenna and holographic antenna arrangement
CN112582784B (zh) * 2020-11-23 2022-03-15 华南理工大学 一种基于环加载和开槽的宽带基站天线及无线通信设备
CN113764894B (zh) * 2021-09-10 2022-10-18 西安电子科技大学 一种三波束独立极化的全息人工阻抗表面天线
GB2616670A (en) * 2022-03-18 2023-09-20 Univ Birmingham Metamaterial-engabled beam scanning antenna

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH088640A (ja) * 1994-06-20 1996-01-12 Toshiba Corp ラジアルラインパッチアンテナ
JP3247155B2 (ja) * 1992-08-28 2002-01-15 凸版印刷株式会社 無給電素子付きラジアルラインスロットアンテナ
JP2012085145A (ja) * 2010-10-13 2012-04-26 Nec Corp アンテナ装置
US20120194399A1 (en) * 2010-10-15 2012-08-02 Adam Bily Surface scattering antennas

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60199201A (ja) * 1984-03-24 1985-10-08 Arimura Giken Kk 円形導波線路
JPH02164108A (ja) * 1988-12-19 1990-06-25 Tokyo Inst Of Technol 平面アンテナ
JP3021752B2 (ja) * 1991-04-26 2000-03-15 凸版印刷株式会社 複合構造ラジアルラインスロットアンテナ
JPH06209214A (ja) * 1992-03-30 1994-07-26 Toppan Printing Co Ltd 直線偏波ラジアルラインスロットアンテナ
WO2004082073A1 (ja) * 1992-12-18 2004-09-23 Naohisa Goto 偏波共用ラジアルラインスロットアンテナ
JPH06314925A (ja) * 1993-04-30 1994-11-08 Toppan Printing Co Ltd 無給電素子付きラジアルラインスロットアンテナおよびそのスロット板の製造方法
JP3356653B2 (ja) * 1997-06-26 2002-12-16 日本電気株式会社 フェーズドアレーアンテナ装置
JP2000341027A (ja) * 1999-05-27 2000-12-08 Nippon Hoso Kyokai <Nhk> パッチアンテナ装置
WO2001071849A2 (en) * 2000-03-20 2001-09-27 Sarnoff Corporation Reconfigurable antenna
US6791497B2 (en) * 2000-10-02 2004-09-14 Israel Aircraft Industries Ltd. Slot spiral miniaturized antenna
JP2003008341A (ja) * 2001-06-22 2003-01-10 Mitsubishi Electric Corp 平面アレーアンテナ
US6674408B1 (en) * 2002-07-19 2004-01-06 Paratek Microwave, Inc. Antenna apparatus
US6842140B2 (en) * 2002-12-03 2005-01-11 Harris Corporation High efficiency slot fed microstrip patch antenna
US7071888B2 (en) * 2003-05-12 2006-07-04 Hrl Laboratories, Llc Steerable leaky wave antenna capable of both forward and backward radiation
JP2007295044A (ja) * 2006-04-20 2007-11-08 Matsushita Electric Ind Co Ltd フェーズドアレイアンテナ
US8013694B2 (en) * 2006-03-31 2011-09-06 Kyocera Corporation Dielectric waveguide device, phase shifter, high frequency switch, and attenuator provided with dielectric waveguide device, high frequency transmitter, high frequency receiver, high frequency transceiver, radar device, array antenna, and method of manufacturing dielectric waveguide device
JP4306734B2 (ja) * 2007-01-31 2009-08-05 カシオ計算機株式会社 平面円偏波アンテナ及び電子機器
US9190735B2 (en) * 2008-04-04 2015-11-17 Tyco Electronics Services Gmbh Single-feed multi-cell metamaterial antenna devices
JP2010068085A (ja) * 2008-09-09 2010-03-25 Toshiba Corp アンテナ装置
FR2959611B1 (fr) * 2010-04-30 2012-06-08 Thales Sa Element rayonnant compact a cavites resonantes.
CN202949040U (zh) * 2012-10-25 2013-05-22 中国传媒大学 起始缝隙距离中心小于一个波导波长的圆极化径向缝隙天线
US9385435B2 (en) * 2013-03-15 2016-07-05 The Invention Science Fund I, Llc Surface scattering antenna improvements
CN103474775B (zh) * 2013-09-06 2015-03-11 中国科学院光电技术研究所 一种基于动态调控人工电磁结构材料的相控阵天线

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3247155B2 (ja) * 1992-08-28 2002-01-15 凸版印刷株式会社 無給電素子付きラジアルラインスロットアンテナ
JPH088640A (ja) * 1994-06-20 1996-01-12 Toshiba Corp ラジアルラインパッチアンテナ
JP2012085145A (ja) * 2010-10-13 2012-04-26 Nec Corp アンテナ装置
US20120194399A1 (en) * 2010-10-15 2012-08-02 Adam Bily Surface scattering antennas

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
ANDO ET AL., RADIAL LINE SLOT ANTENNA FOR 12 GHZ DBS SATELLITE RECEPTION
RADU MARIN: "Investigations on liquid crystal reconfigurable unit cells for mm-wave reflectarrays", 1 January 2008 (2008-01-01), pages i - 155, XP055401196, Retrieved from the Internet <URL:http://tuprints.ulb.tu-darmstadt.de/1089/1/diss_Radu_Marin_WebPubl.pdf> [retrieved on 20170825] *
YUAN ET AL., DESIGN AND EXPERIMENTS OF A NOVEL RADIAL LINE SLOT ANTENNA FOR HIGH-POWER MICROWAVE APPLICATIONS

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KR20160130975A (ko) 2016-11-15
ES2935284T3 (es) 2023-03-03
ES2856220T3 (es) 2021-09-27
WO2015126550A1 (en) 2015-08-27
KR101864052B1 (ko) 2018-06-01
EP3800735B1 (de) 2022-11-16
EP4191794A1 (de) 2023-06-07
CN110492238B (zh) 2021-02-09
CN105960735A (zh) 2016-09-21
CN105960735B (zh) 2019-09-17
CN110492238A (zh) 2019-11-22
BR112016018882A2 (pt) 2020-10-27
TW201541714A (zh) 2015-11-01
EP3108538A1 (de) 2016-12-28
TWI634701B (zh) 2018-09-01
EP3108538A4 (de) 2017-10-11
BR112016018882B1 (pt) 2022-02-22
EP3108538B1 (de) 2020-12-23
JP2017506471A (ja) 2017-03-02

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