Systems and methods for designing, optimizing, patterning, forming, and manufacturing symphotic structures are described herein. A symphotic structure may be formed by identifying a continuous refractive index distribution calculated to convert each of a plurality of input reference waves to a corresponding plurality of output object waves. The continuous refractive index distribution can be modeled as a plurality of subwavelength voxels. The system can calculate a symphotic pattern as a three-dimensional array of discrete dipole values to functionally approximate the subwavelength voxels. A symphotic structure may be formed with a volumetric distribution of dipole structures. A dipole value, such as a dipole moment (direction and magnitude) of each dipole is selected for the volumetric distribution to convert a plurality of input reference waves to a target plurality of output object waves.

To accurately estimate frequency characteristics from structural parameters of a frequency selective surface. A frequency selective surface design apparatus includes an LC generation unit 20 that receives an input of a structural parameter, and generates an inductance L and a capacitance C of a unit cell, a corrected resonance point calculation unit 30 that receives the number n of times of calculation input from an outside, the inductance L, and the capacitance C, models a correction circuit by using a circuit in which a virtual capacitance is connected in parallel via a transmission line to each distribution inductance obtained by division of the inductance L by the calculation number n and the transmission line is terminated at the capacitance C, and calculates a corrected resonant frequency fC from the impedance of the correction circuit, and a characteristic calculation unit 40 that receives inputs of the inductance L, the capacitance C, and the corrected resonant frequency fC, calculates a pre-correction resonant frequency from the inductance L and the capacitance C, obtains a correction coefficient by dividing the corrected resonant frequency fC by the pre-correction resonant frequency, and calculates a corrected return loss and a corrected insertion loss.

A method of conforming a periodic array to a surface is provided. The method comprises calculating, with a spatially-variant lattice algorithm, a pair of planar gratings across the surface, wherein the planar gratings are generated via reciprocal lattice vectors and summing the pair of planar gratings. Intersections produced by summing the gratings are scanned for maxima on the surface, and a periodic array of elements is located at the maxima on the surface. A normal vector is calculated at each maximum on the surface, and each element is rotated to match the direction of the respective normal vector at each maximum on the surface. The elements are then conformed to the surface via a shrink-wrap modifier operation.

The present invention discloses a reconfigurable wideband phase-switched screen (PSS) based on an artificial magnetic conductor (AMC). Gap capacitance between patches is controlled by changing the capacitance of varactors, so that periodic units have a plurality of continuous frequency points. A phase difference between two adjacent frequency bands is 143°-217°, so that the periodic structure absorbs incident electromagnetic waves in a wide frequency band, and the broadband PSS is implemented with a relative bandwidth of 45.2%. The AMC structure according to the present invention is simple in structure and easy to process, with a thickness less than one twentieth of the working wavelength, and greatly reduces size and costs.

A scattering device 10 is described comprising a plurality of dipoles 20, each comprising a rod and a pair of plates 12, 22, the plates 12, 22 being located at the respective ends of the rod, the rods of the dipoles 20 being connected to one another and arranged such that the rods are angled relative to one another.

Antenna arrays with three-dimensional (3D) radiating elements are provided, as well as methods of manufacturing and methods of using the same. An array can include a ground plane and a plurality of radiating elements disposed thereon, and at least a portion of the radiating elements of the plurality of radiating elements can be 3D radiating elements. The array can optionally include a substrate disposed on the ground plane and having holes for the radiating elements. The 3D radiating elements can include, for example, conical elements such as a hollow conical element, a full conical element, a hollow and discretized conical element, or a combination thereof.

An array antenna (A) in a medium (M) comprises a plurality of radiating elements (ER.sub.T) ensuring the transition between the antenna and the medium, the reflectivity of each element depending on a parameter, the reflectivity of a first element being close to that of the medium, the reflectivity of a last element being close to that of the antenna, the reflectivity parameter of the elements varying from one element to the next. A method comprises calculation of a path equal to the sum of the variations of the reflectivity from one element to the next element, optimization of the variation of the reflectivity parameter so that equivalent radar cross-section of the antenna is the lowest possible or the antenna best observes the radiation objectives, determination of the different elements as a function of said parameter, and simulation of the overall reflectivity and/or of the radiation of the antenna.

A signal isolation device includes at least one electromagnetic band-gap unit. The at least one electromagnetic band-gap unit includes a substrate, a metal foil main body, and a plurality of T-shaped metal foil features. The metal foil main body is disposed on the substrate, and the metal foil main body is square. The T-shaped metal foil features is disposed on the substrate and extending from a periphery of the metal foil main body. The T-shaped metal foil features are in a rotational symmetry around a center of the metal foil main body.

A process for manufacturing a composite material of 3-D shape, includes a stack of layers of resin and fibre, incorporating at least one metal layer, the process comprising the following steps, a standard unit pattern having been determined for the metal layer: i/computing periodically organized patterns on the 3-D shape, which is non-developable; then projecting, onto a plane, the patterns, thus defining a planar organization of second patterns; ii/partially polymerizing, flat, first layers, comprising a metal top layer, of the flat composite stack, so as to make it etchable, but to keep it still deformable; iii/electrochemically etching the organization of second patterns that was defined in step i into the metal top layer of the flat composite stack resulting from step iv/carrying out polymerization of the etched composite stack after the stack has been placed in a mould having the desired 3-D shape.

To accurately estimate frequency characteristics from structural parameters of a frequency selective surface. A frequency selective surface design apparatus includes an LC generation unit 20 that receives an input of a structural parameter, and generates an inductance L and a capacitance C of a unit cell, a corrected resonance point calculation unit 30 that receives the number n of times of calculation input from an outside, the inductance L, and the capacitance C, models a correction circuit by using a circuit in which a virtual capacitance is connected in parallel via a transmission line to each distribution inductance obtained by division of the inductance L by the calculation number n and the transmission line is terminated at the capacitance C, and calculates a corrected resonant frequency fC from the impedance of the correction circuit, and a characteristic calculation unit 40 that receives inputs of the inductance L, the capacitance C, and the corrected resonant frequency fC, calculates a pre-correction resonant frequency from the inductance L and the capacitance C, obtains a correction coefficient by dividing the corrected resonant frequency fC by the pre-correction resonant frequency, and calculates a corrected return loss and a corrected insertion loss.