Cubesat missions for low-earth orbit have seen significant growth over the last decade offering new opportunities to expand space exploration. Two of their main advantages are their short design time and low fabrication cost. Space communication systems require High Gain Antennas (HGAs), such as Reflectarray Antennas (RAs), and parabolic reflectors. Foldable panel RAs are the most commonly used concept for CubeSat HGAs; they offer small stowed volume, low mass, and low cost. However, these RAs radiate in only one pre-defined direction while many applications require communications in multiple directions.
Implementing beamsteering techniques in Cubesat RAs is quite challenging because it introduces losses, increases cost, and requires high power. In addition, previously proposed foldable panels have not been reconfigurable and they are usually attached to one another using spring-loaded hinges, which require longer assembly times and a larger number of components, thereby increasing the production cost of RAs
Embodiments of the subject invention provide novel and advantageous arrays that are deployable and can change their electromagnetic behavior by changing their shape. An array can include a central panel and at least one foldable panel attached thereto. The central panel can include at least one radiating element on its upper surface while each foldable panel can have at least one radiating element on its bottom surface. The array is reconfigurable where each foldable panel can be folded onto the central panel such that its bottom surface then faces upward and covers (and thereby “replaces” for the purposes of radiating) part or all of the upper surface of the central panel. By including more foldable panels attached to the central panel, more configurations can be achieved where different foldable panels and/or different combinations of foldable panels can be folded onto the central panel to give different combinations of radiating elements facing upward. The foldable panels can be attached to the central panel via any suitable means, including for example hinges or creases in the substrate.
Any suitable actuation system can be used to fold and unfold the foldable panels, and the foldable panels and the central panel can each have any suitable shape (e.g., rectangular, triangular, square).
In an embodiment, an array can comprise: a central panel comprising an upper surface, a bottom surface opposite from the upper surface, and a first plurality of radiating elements disposed on the upper surface; and at least one foldable panel foldably attached to the central panel and comprising an upper surface, a bottom surface opposite from the upper surface, and a respective plurality of radiating elements disposed on the bottom surface. Each foldable panel can be foldable such that it is capable of: folding onto the upper surface of the central panel and having the bottom surface thereof face the upper surface of the central panel; and folding onto the bottom surface of the central panel and having the upper surface thereof face the bottom surface of the central panel. The array can be a reflectarray or a phased array. In the case of a reflectarray, the upper surface and/or the bottom surface of the central panel can be a full ground plane. The array can further comprising a plurality of hinges, and each foldable panel can be respectively attached to the central panel by a hinge of the plurality of hinges. The at least one foldable panel, the central panel, and the plurality of hinges can be monolithically formed with each other. A material of the substrate of the central panel can be the same as that of the respective substrate of each foldable panel. The respective pluralities of radiating elements of the at least one foldable panel can be configured such that different patterns of radiating elements are formed by folding different combinations of foldable panels onto the upper surface of the central panel.
In another embodiment, a method for changing the electromagnetic properties (including but not limited to the frequency of operation, the polarization, and the beam direction) of an array can comprise: providing an array as described herein; and folding at least one foldable panel onto the upper surface of the central panel such that the bottom surface of the at least one first foldable panel faces the upper surface of the central panel, thereby having the plurality of radiating elements of the at least one foldable panel be visible from a point of view above the upper surface of the central panel and changing the electromagnetic properties of the array. The electromagnetic properties can include but are not limited to the frequency of operation, the polarization, and the beam direction). In a further embodiment where the array has four foldable panels, the method can comprise: folding first and second foldable panels onto the upper surface of the central panel and having the bottom surfaces thereof face the upper surface of the central panel, thereby having the pluralities of radiating elements thereof be visible from the point of view above the upper surface of the central panel; folding a third foldable panel onto the bottom surface of the central panel and having the upper surface thereof face the bottom surface of the central panel; and folding a fourth foldable panel onto the bottom surface of the central panel and having the upper surface thereof face the bottom surface of the central panel. Such a method can further comprise: folding the first and second foldable panels onto the bottom surface of the central panel and having the respective upper surfaces of the first and second foldable panels face the bottom surface of the central panel; and folding the third and fourth foldable panels onto the upper surface of the central panel and having the respective bottom surfaces thereof face the upper surface of the central panel, thereby having the respective pluralities of radiating elements thereof be visible from the point of view above the upper surface of the central panel and changing the electromagnetic properties (e.g., the frequency of operation, the polarization, and/or the beam direction) of the array.
Embodiments of the subject invention provide novel and advantageous arrays that are deployable and can change their electromagnetic behavior by changing their shape. An array can include a central panel and at least one foldable panel attached thereto. The foldable panels can be monolithically formed with the central panel, though embodiments are not limited thereto. The central panel can include at least one radiating element on its upper surface while each foldable panel can have at least one radiating element on its bottom surface. The array is reconfigurable where each foldable panel can be folded onto the central panel such that its bottom surface then faces upward and covers (and thereby “replaces” for the purposes of radiating) part or all of the upper surface of the central panel. By including more foldable panels attached to the central panel, more configurations can be achieved where different foldable panels and/or different combinations of foldable panels can be folded onto the central panel to give different combinations of radiating elements facing upward. The foldable panels can be attached to the central panel via any suitable means, including for example hinges or creases in the substrate. Any suitable actuation system can be used to fold and unfold the foldable panels, and the foldable panels and the central panel can each have any suitable shape (e.g., rectangular, triangular, square).
Arrays of embodiments of the subject invention can steer their beam or change their polarization or operation frequency by using different combinations of folds of the foldable panels. The arrays can achieve multiple operation states by reconfiguring their structure through folding of the foldable panels. The term “array” as used herein refers to phased arrays and reflectarrays. Any suitable substrate (rigid or flexible) can be used for the arrays, including but not limited to Duroid, FR4, or Kapton. Any conductive material can be used for the arrays, including but not limited to copper, aluminium, silver, gold, or platinum.
A reflectarray is an antenna with a flat or slightly curved reflecting surface and an illuminating feed antenna. Many radiating elements are typically present on the reflecting surface. The feed antenna spatially illuminates the radiating elements that are designed to reradiate and scatter the incident field with electrical phases that are required to form a planar phase front in the far-field distance. Several methods can be used for reflectarray elements to achieve a planar phase front.
Referring still to
In Case 1, the central panel steers its beam in the broadside direction (θ=0°, φ=0°); in Case 2, the array steers the beam in the direction θ=−30°, φ=0°; and in Case 3, the array steers the beam in the direction θ=30°, φ=0°.
The array shown in
The foldable panels can be attached to the central panel via any suitable means, including for example hinges or creases in the substrate. For example, hinges can be used and can be made using the same substrate material as the central panel and the foldable panels. That is, the hinge(s) can be formed by making slots or other gaps in the material to make it bendable, such that the central panel, the hinge(s), and the foldable panel(s) are monolithically formed.
Embodiments of the subject invention can reconfigure their electromagnetic characteristics and can also be efficiently packed. The arrays can change their shape through folding, enabling them to reconfigure performance and provide multi-functionality, such that the user can direct the beam in the desired direction and not have to rely only on the electronic configuration that is conventionally used. The arrays can reconfigure their electromagnetic performance (e.g., beamsteering, polarization reconfigurability, frequency reconfigurability) by folding a combination of the foldable panels to change the electromagnetic design (layout). Use of such arrays provides new capabilities to communication systems (e.g., satellite communications systems). Embodiments of the subject invention can be used in several fields, including but not limited to multi-functional communications, satellite communication systems, and deployable, packable, and collapsible arrays.
A greater understanding of the embodiments of the subject invention and of their many advantages may be had from the following examples, given by way of illustration. The following examples are illustrative of some of the methods, applications, embodiments, and variants of the present invention. They are, of course, not to be considered as limiting the invention. Numerous changes and modifications can be made with respect to the invention.
A reconfigurable monolithic reflectarray with foldable panels was designed and tested. The reflectarray had a central panel and two foldable panels (each approximately one half of the width of the central panel), such that at least three different configurations can be used, as shown in
The properties of the reflectarray were determined using a simulation with ANSYS HFSS with master-slave boundaries.
Two surrogate hinges were introduced in the design to make the reflectarray foldable, as seen in
For design simplification, two foldable panels were used. A linearly polarized horn is placed at 8.7λ from the center of the reflectarray with an offset of 20° in the yz plane. The required phase shift of the elements on each aperture was calculated using the ray-tracing method. Two pencil beams focused in (θ=30°, φ=0°) and (θ=−30°, φ=0°) were designed for RA1 and RA2, respectively. Two combinations were possible for the dual-beam operation, one being the right panel of RA2 folded up and the left panel down, or the opposite.
A prototype of the reflectarray example was manufactured in a single step using standard PCB fabrication. The different folding states of the reflectarray, namely, RA1, RA2, RA12, and RA21 are depicted in
The performance of the fabricated RA was measured using an MVG Starlab system.
It should be understood that the examples and embodiments described herein are for illustrative purposes only and that various modifications or changes in light thereof will be suggested to persons skilled in the art and are to be included within the spirit and purview of this application.
All patents, patent applications, provisional applications, and publications referred to or cited herein are incorporated by reference in their entirety, including all figures and tables, to the extent they are not inconsistent with the explicit teachings of this specification.
This invention was made with government support under Award Number FA9550-18-1-0191 awarded by the Air Force. The government has certain rights in the invention.
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8289221 | Finucane | Oct 2012 | B1 |
20080143636 | Couchman | Jun 2008 | A1 |
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