In recent years, the increasing data volume shared over terrestrial to satellite communication links triggered the demand for higher capacity channels. This resulted in the need for wider bandwidth communication systems.
In addition, the use of CubeSats for cheaper and wider communication coverage opened the possibilities for cluster satellite communication. Thus, since CubeSats are small, they require miniaturized and light antennas.
In space applications and specifically on CubeSat satellites, a K/Ka-band printed antenna is desired. The antenna should be easily assembled and placed. Moreover, the antenna needs to operate with high purity circular polarization in order to avoid wave depolarization while propagating through the atmospheric media. Furthermore, good communication links with the earth terminal stations can be established and secured with high gain antennas.
Planar antenna arrays with broadside a radiation pattern is preferred as a low-profile structure. Such a structure can support any kind of polarization. This is determined by the radiating element shape, the arrangement of the elements and the feeding method used. It also allows for high gain by proper element positioning.
In other efforts, circular polarization is created by implementing truncated rectangular patches with a narrow circular polarization tendency band. This design has the elements orthogonally oriented between each other and fed by a combination of a sequential rotation and a parallel feeding network to form an n-element antenna array.
A different technique that has been implemented previously is the use of wideband linearly polarized elements placed in cross configuration and fed by double sequential feeding network to excite circular polarization.
Another effort for circular polarization is the feeding of a 4×4 circular patch array through modified aperture slot arms. The stacked antenna has a parallel feeding network at its bottom that feeds the radiating elements in phase through coupling.
In one embodiment, the present invention concerns the design of miniaturized compact antennas.
In another embodiment, the present invention provides antennas that support the lowest axial ratio currently possible, have a highly directional pattern with the lowest side lobe level and have an extremely large operating range limited only by the desired performance.
In another embodiment, the present invention provides a wideband right hand circularly polarized antenna array having sequential rotation power dividers; a stack assembly topology; and continual orthogonal placement of the elements.
In another embodiment, present invention provides a wideband right hand circularly polarized antenna array based on the implementation of sequential rotation power dividers. The antenna characteristics and footprint are improved by using a stack assembly topology and a continual orthogonal placement of the elements.
In the drawings, which are not necessarily drawn to scale, like numerals may describe substantially similar components throughout the several views. Like numerals having different letter suffixes may represent different instances of substantially similar components. The drawings illustrate generally, by way of example, but not by way of limitation, a detailed description of certain embodiments discussed in the present document.
Detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention, which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed method, structure or system. Further, the terms and phrases used herein are not intended to be limiting, but rather to provide an understandable description of the invention.
Thorough the below description of the various embodiments of the present invention, one or more models or examples will be provided. However, the methodology remains the same to secure the aforementioned traits of various antennas.
In one embodiment, the present invention provides a K/Ka-band wideband right hand circularly polarized 16-element stack antenna array 100 fed by sequential rotation series power dividers as shown in
As shown in
As also shown in
In a preferred embodiment, as further shown in
In other aspects, the present invention provides one or more truncated rectangular patches that create an elliptical polarized dual-band element, with center frequencies far apart from each other. In one embodiment, the center frequencies are 23 GHz and 29.8 GHz. The advantage of this embodiment is the acquisition of a radiating element with circular polarization and wideband operation tendency that can be later on exploited while forming a 16-element antenna array. In other words, it is close to impossible to design a printed single element that can operate in large bandwidths with circular polarization behavior. Thus, this approach uses an elliptical polarized base radiating element having the tendency of these features. In addition, improved performance, such as bandwidth and circular polarization traits, is achieved by combining the single element with a sequential rotational series feeding network.
The sequential rotational series feeding network provides wideband power distribution to the output ports. An advantage of using such a divider is that the series configuration can provide 90° phase difference between its output ports at the desired frequency. The other advantage is the rotational formation that permits size reduction and an orthogonal configuration between the connecting elements.
In another aspect, microwave transmission line analysis along with circuit analysis may be performed to determine the different impedances of the different transmission lines of the divider for matching techniques, equal power distribution and size reduction, as
The input impedance of the power divider is desired to be 50 Ohm while the output ports are to be around 135 Ohm, the impedance seen from the truncated patches. As shown in
The main feed network of the array is implemented at the bottom layer and the connection to the group array is done through VIAs, as
Furthermore, once the 4 elements are connected to the power divider, the divider's sections are tuned to create a wideband radiator (the group array), with an extra improvement of the circular polarization purity.
The 4-group array of the preferred embodiment of the present invention may be implemented at the top layer of the stack antenna incorporating 16 elements. These groups are fed through VIAs from the bottom of the stack. Each VIA has 0.1 mm radius and passes through 0.2 mm radius ground holes. The ground plane is sandwiched between the top and bottom substrates. The bottom substrate is an RT5870 with 0.13 mm thick slab with a relative permittivity of 2.33 and hosts the main feeding network.
As shown in
The preferred embodiment of the present invention provides a 16-element circularly polarized antenna array that is a compact miniaturized stack antenna with exceptional characteristics. The embodiment has a reflection coefficient less than −20 dB at the frequency range of interest (21-31 GHz). The antenna operating range extends more than the above-mentioned range, as
The gain produced by the array is 12-15 dB at frequencies between 21-30.8 GHz. The gain peaks are situated at the resonant frequencies of the dual-band over-truncated elliptically polarized single element, as shown in
The axial ratio of the antenna array is less than 0.5 dB at frequencies between 21.5-30 GHz, while above 0.5 dB is extended beyond 31 GHz, as shown in
The cross-polarization discrimination between RHCP and LHCP that is produced by the current model is at least 25 dB, as shown in
The radiation efficiency of the antenna is more than 95% at the frequency range 21-30.5 GHz, as shown
The radiation pattern of the array at 23 GHz shows a side lobe level (SLLs) lower than 20 dB in the plane Φ=0° and a SLL lower than 17.5 dB in the plane Φ=90°. The radiation pattern of the array at 26.25 GHz shows a side lobe level lower than 20 dB in the plane Φ=0° and a SLL lower than 15 dB in the plane Φ=90°. The radiation pattern of the array at 28.75 GHz shows a side lobe level lower than 17.5 dB in the plane Φ=0° and a SLL lower than 17 dB in the plane Φ=90° as seen in
The embodiments of present invention insure wideband characteristics such as reflection coefficient, axial ratio, high gain, low side lobes and high efficiency, through a series of methodical steps. The total size of the antenna is 52×32 mm. Thus, the final model is a miniaturized antenna for CubeSat operations.
While the foregoing written description enables one of ordinary skill to make and use what is considered presently to be the best mode thereof, those of ordinary skill will understand and appreciate the existence of variations, combinations, and equivalents of the specific embodiment, method, and examples herein. The disclosure should therefore not be limited by the above-described embodiments, methods, and examples, but by all embodiments and methods within the scope and spirit of the disclosure.
This application claims priority to U.S. Provisional application Ser. No. 62/781,530 filed on 18 Dec. 2018, which is incorporated herein in its entirety.
This invention was made with government support by the National Aeronautics and Space Administration grant number NNX17CC01C. The government has certain rights in the invention.
Filing Document | Filing Date | Country | Kind |
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PCT/US2019/066391 | 12/13/2019 | WO | 00 |
Number | Date | Country | |
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62781530 | Dec 2018 | US |