Introduction
Nowadays, the demand for wireless communications with high capacity and good adaptability is growing rapidly. Due to the limitation of available spectrum resources, orbital angular momentum (OAM) technology is considered as a potential choice in wireless communications, which can remarkably increase the capacity with low crosstalk on the same frequency under certain conditions [1], [2]. As a key component, the antennas with switchable operating states are capable of adapting the sudden change including pattern, polarization, or other performances to enhance their robustness [3]–[5]. With the attractive features mentioned above, the design of OAM reconfigurable antennas has become a topic of concern in recent years.
Up to now, various types of antenna have been used to generate radio beams with OAM vortices, including spiral phase plate (SPP) [6], [7], dielectric resonator antenna (DRA) [8], eigenmode-based antenna [9]–[11], metasurface [12]–[16], and uniform circular array (UCA) [17]–[19]. However, some antennas [6]–[9] can only produce one fixed OAM mode corresponding to a specific structure. In [10]–[14], their physical structures or dimensions must be changed with OAM modes, thus these antennas are not suitable for the adjustable characteristics. The programmable metasurfaces have the potential for flexible OAM-waves generation. An efficient reconfigurable transmissive metasurface [15] is exploited to produce tunable multimode OAM beams. A reflective metasurface loaded with varactor diodes is also applied for realizing mode reconfigurability [16]. However, there exists a large amount of switches and lumped components in these reconfigurable metasurfaces. In addition, it is difficult to integrate their 3D structures within the planar circuits. Alternatively, the UCAs facilitate phase control of the elements, which makes them a good candidate for reconfigurable antenna designs [20]–[27]. The antenna arrays [21], [22] enable OAM-mode manipulation with the aid of a reconfigurable feed network (RFN). A mechanically reconfigurable array with single-arm spiral antennas is used to generate broadband circularly polarized vortex waves [23]. By using sequentially rotated feed technique, the antenna [24] with two feed networks can radiate dual CP dual-mode OAM beams, which are controlled by switching the excitation ports. However, most antennas mentioned above suffer from limitations such as complex feed network, slow tuning speed, or single parameter reconfigurability.
In this paper, a dual-mode and dual-circular-polarization compound reconfigurable patch array antenna for generating vortex beams is presented. It is constructed based on a UCA of four multi-functional elements, which offers polarization switching between left-hand CP (LHCP) and right-hand CP (RHCP) as well as provides specific initial phases to simplify the feed structure. By controlling the embedded radio frequency (RF) switches, the initial phases are superimposed with an additional and tunable +90° or −90° phase shift. As a result, the total excitation phases satisfy the phase requirements for achieving both OAM-mode
Antenna Design and Analysis
A. Design Scheme
The generation of OAM beams with a UCA requires feeding the antenna elements with equal amplitude but a successive phase delay. In the four-element UCA (denoted by Ant. 1) at Cartesian coordinates (
The realization of the four-element array with both tunable circular polarizations and OAM modes still faces two main challenges. The first one lies in the allocation of different phases to different elements in the same direction, for example −90°, 0°, −90°, and 0° are separately required to allocated to E1, E2, E3 and E4 in
To resolve these challenges, the total antenna array is constructed with an orthogonal arrangement, allowing to form different phases for different elements in one direction. Furthermore, the antenna elements could also be designed tunable feed ports as well as a phase-shifting feedline. Switching the feed ports helps to alter the orientation of antenna currents, and properly selecting the lengths of the corresponding feedlines further results in a switchable phase difference between ports. In this way, the phase requirements for different directions of each element could be satisfied.
B. Antenna Configuration
Based on the design idea, the configuration of the proposed array antenna is shown in Fig. 2. The antenna is located at the Cartesian coordinate system Oxyz, in which each element is rotated by 45° anticlockwise around
Configuration of the proposed antenna array. (a) Side view. (b) Top view. (c) Zoomed-in view of antenna element (Unit: mm).
In the bias circuit of p-i-n diodes, the anodes are attached to the individual bias pads while cathodes to the common ground. By switching the probes and corresponding feedlines, dual feed with a counterclockwise −90° (+90°) or −90° phase difference are selected for exciting the element, and thus LHCP or RHCP reconfigurability can be realized. Moreover, thanks to the orthogonal arrangement and switchable dual-feed method, the required phases for both OAM-mode and polarization reconfigurability can be fulfilled without additional reconfigurable feed network.
The performance of antenna array is investigated through simulation. In the simulation using ANSYS HFSS, the equivalent circuit models of the p-i-n diodes (SMP1345-040LF from Skyworks) for ON/OFF status are incorporated. As plotted in Fig. 3, they are modeled as an inductance of
Simulated surface current distributions of the antenna array for state 1 at 2.5 GHz.
In Fig. 5(a), the simulated reflection coefficients indicate that the antenna array exhibits an overlapped impedance bandwidth with
(a) Simulated reflection coefficients of the array antenna. (b) Simulated ARs of the antenna array.
The near-field phase distributions for the four operating states are plotted in Fig. 6. As can be seen, the phase changes
Experimental Results and Discussions
A. Antenna Fabrication
Based on the design and analysis, an antenna prototype is manufactured, as shown in Fig. 7. The prototype mainly consist of a sandwich-like structure on a three-layered printed circuit board (PCB) and four circular patches on single-layered PCBs. In the sandwich-like structure, the ring patches serving as driven radiators are printed on the upper layer. Their feed lines as well as the total 1:4 power divider of the array are fabricated on the lower layer. The bias circuits including the shoring vias and bias pads are arranged beside the feed lines. In addition, a common ground plane is vertically sandwiched between the upper and lower layers. To prevent short circuits while feeding energy to the upper ring patches, part of ground plane is demetallized for the feed probes to pass through. The circular substrates with parasitic radiators located at top are supported by plastic holders. To facilitate the switching of bias configurations, a control board realized on a 1mm-thickness FR4 substrate is placed beneath the bias circuit. With the aid of a microcontroller, the appropriate direct current (dc) bias voltages for the reconfigurable states can be produced as listed in Table 2. The generated control signals are delivered to the bias circuit through flexible wires. Assembled with plastic screws, the entire array has overall dimensions of
Photographs of the fabricated prototype. (a) Middle layer. (b) Bottom layer. (c) Control board. (d) Assembled antenna.
B. Reflection Coefficients and Axial Ratios
Measured reflection coefficients of the proposed antenna array are plotted in Fig. 8(a). The operating states are chosen according to those defined in Table 2. It is indicated that the measured bandwidth with
(a) Measured reflection coefficients of the array antenna. (b) Measured 3-dB AR bandwidths in xoz - and yoz - planes at 2.5 GHz.
C. Near-Field Distributions
Spiral electric field distributions are typical characteristics of vortex electromagnetic waves, which can be investigated by examining the near-field phase and intensity distributions. The measurement are implemented with a two-dimensional scanning system in the anechoic chamber, as displayed in Fig. 9. The distance between the measured antenna and observed surface is 500 mm, which is about
It is clearly that at all states, there exists intensity nulls in the broadside direction, forming a hollow structure similar to a donut. It also can be seen that the phases of the electric field at states 1 and 3 are distributed along a circular path around the z-axis and change
The normalized far-field radiation patterns in the xoz- and yoz- planes at 2.5 GHz are shown in Fig. 12. Due to the symmetry of the structure, the divergence angles at which the maximum co-polarization gain occurs of all states show good consistency. It can be found that there is an amplitude null in the propagation direction due to the helical phase profile. Moreover, it is seen that the proposed antenna can produce dual-polarization properties, namely, LHCP and RHCP. It is also found from these figures that the measured cross-polarization discriminations are kept below −20 dB.
Finally, Table 3 compares the performance of the proposed reconfigurable OAM antenna with other referenced works. As indicated, the proposed antenna has superior performance in arbitrarily switching operating states between two circular polarizations while maintaining a relatively simple antenna structure. Moreover, the proposed antenna array supports the element phase reconfiguration. It is expected that this method could be extended to larger elements antenna array to generate higher order OAM waves without extra phase-shifting network.
Conclusion
In summary, a dual OAM modes and dual CPs reconfigurable antenna array is designed, fabricated, and measured. The antenna array is constructed based on a UCA of four dual-fed elements, each of which provides a quadrature phase difference between adjacent feed ports. By properly selecting feed probes of each element and arranging the elements orthogonally, the required phases for dual CPs and dual OAM modes can be achieved simultaneously. Measured results indicate that the fabricated antenna prototype achieves four operating states with OAM mode