Low-profile Circularly Polarized Conformal Antenna Array with Side Lobe Suppression for Vehicular SATCOM Applications
Ebenezer Abishek, Ramesh Subramaniam, Parthasarathy Ramanujam, and Manikandan Esakkimuthu
1Department of Electronics and Communication Engineering
Vel Tech Multi Tech Dr.Rangarajan Dr.Sakunthala Engineering College, Chennai, 600062, India
ebenezerabishek@gmail.com
2Department of Electronics and Communication Engineering
SRM Valliammai Engineering College, Chennai, 603203, India
3Department of Electronics and Communication Engineering
National Institute of Technology, Tiruchirappalli, 620015, India
4Centre for Innovation and Product Development
Vellore Institute of Technology, Chennai, 600127, India
Submitted On: October 21, 2022; Accepted On: July 1, 2023
A circularly polarized microstrip antenna array with low side lobe levels is proposed for Vehicular Satellite Communication. The suppression of side lobe levels is accomplished by the non-uniform power distribution utilized to feed the individual patch elements. Impedance matching is ensured by the incorporation of a quarter-wave transformer via a microstrip line fed to the edge of the patch. When the proposed amplitude-weighted feed is compared to the conventional corporate feed, simulation results indicate a reduction in side lobe levels of 8.9 dB. The proposed antenna is constructed out of RT/DUROID 5880 material, which is lighter, more flexible, and less expensive than ceramic materials. The radiation characteristics of the proposed antenna are compared when the antenna is planar versus when it is made to conform to the roof of the vehicle. The measured results indicate a reflection coefficient at the resonant frequency of -31.5 dB and -27.7 dB when conformal, an impedance bandwidth of 410 MHz and 180 MHz when conformal, an axial ratio bandwidth of 140 MHz and 170 MHz when conformal, and a peak gain of 15.719 dB and 14.335 dB when conformal. The measured results validate the simulation results that this proposed antenna is appropriate for a variety of Vehicular Satellite Communication applications.
Index Terms: amplitude tapering ratio, circular polarization, microstrip array, side lobe level, vehicular satellite communication.
The vehicle-based SATCOM technology is known as Vehicular Satellite Communication. Satellites are utilized to establish and maintain communication between moving vehicles and immobile infrastructures such as hospitals, police stations, etc. Compared to vehicle-to-vehicle communication, the satellite provides a larger coverage area in vehicular satellite communication [1]. Important issues that must be addressed in Vehicular Satellite Communication include interference with nearby satellites [2], [3] and the need for increased power to provide high-quality services [4], [5]. Due to their ability to overcome the Faraday rotation that occurs in the ionosphere, circularly polarized antennas are preferred for Vehicular Satellite Communications [6], [7]. The radiation characteristics of a microstrip antenna with a single element can be enhanced by constructing an array of that antenna.
Microstrip technology is used to develop the proposed antenna as a low-profile alternative to conventional SATCOM antennas. IEEE has established Wireless Access in Vehicular Environment as the standard for vehicular networks [8], [9]. This standard is a part of the IEEE 802.11p protocol for mobile ad hoc networks. Vehicular Satellite Communication necessitates the installation of antennas on moving vehicles. More than 50% of earth-orbiting satellites are used for communication [10], [11]. Among these satellites there are satellites used exclusively for Vehicular Satellite Communication to connect moving vehicles and also to stationary infrastructures [12], [13]. There are numerous civilian applications, including the use of laptops or mobile devices with high-speed internet connectivity in moving vehicles, rapid rescue of passengers in moving vehicles in the event of an accident, tracking of thieves travelling in moving vehicles in the event of a theft, etc. [14]. Vehicular Satellite Communication antennas are also required for military vehicles to maintain communication with the satellite even when traversing difficult terrain [15], [16]. There is a need for low-profile alternatives to high-profile vehicular antennas because a greater number of antennas must be integrated into vehicles as the number of applications increases [17].
Power is a crucial factor for providing high-quality services in moving vehicles. Therefore, it is undesirable for the side lobes to waste energy. Various techniques can be used to suppress side lobes [18]. To address this issue, it is proposed to implement a feed structure that suppresses the side lobes, thereby reducing the battery’s power consumption. This feed structure is incorporated into the proposed planar antenna array alongside circularly polarized patches. The radiation characteristics of this proposed planar antenna array are examined and discussed.
The antenna proposed was developed in three stages. In the initial phase of the work, a single element microstrip antenna with circular polarization and improved cross polarization isolation is developed. This preliminary phase of the project has been completed and published [19]. A proposed feed structure is designed to suppress the side lobes in the second stage. Using the single element circularly polarized microstrip patch antenna developed in the first stage and the proposed feed structure, a proposed 18 element antenna array is constructed. The third stage entails adapting the proposed planar antenna array to the shape of the vehicle’s roof. The antenna’s dimensions are optimized to compensate for changes in the desired performance caused by the conformal placement of the proposed antenna on the roof of the vehicle. The proposed antenna’s radiation characteristics are analyzed using both simulated and measured data.
The proposed feed structure uses unequal T-junction power dividers to distribute power with tapered amplitude. Taylor, Chebyshev, and Binomial arrays are frequently employed amplitude tapered or amplitude weighted arrays, each with their own benefits and drawbacks. Although Binary arrays completely eliminate side lobes, the amplitude coefficients of the array’s individual elements vary greatly. If the Taylor array achieves a radiation pattern with complete suppression of inner side lobes and all side lobes at the same level, directivity will decrease. Chebyshev arrays are also used to obtain optimal main lobe and suppressed side lobe radiation patterns. The T-junction used for unequal power distribution is shown in Fig. 1.
Assuming lossless transmission, the relation between input and output power of the T-junction power divider for unequal power distribution can be written as
(1) | ||||
(2) | ||||
(3) | ||||
(4) | ||||
(5) |
where a value lies between 0 and 1.
The output port impedances derived from the above equations can be written as
(6) | ||||
(7) |
Parameters | Values |
---|---|
Lg Wg | 39.23mm 157.83mm |
Lp Wp | 8mm 8mm |
Dc | 1.2 |
Dx | 0.69 |
Lf Wf | 4mm 2mm |
L1 W1 | 0.4mm 60mm |
L2 W2 | 1.2mm 4.8mm |
L3 W3 | 2.4mm 2mm |
L4 W4 | 1.1mm 10.8mm |
L5 W5 | 1.7mm 4.9mm |
L6 W6 | 2.5mm 2mm |
L7 W7 | 0.5mm 5.5mm |
L8 W8 | 1.4mm 4.9mm |
L9 W9 | 7.8mm 2mm |
L10 W10 | 5.6mm 0.4mm |
L11 W11 | 0.15mm 11mm |
L12 W12 | 0.85mm 4.9 |
L13 W13 | 2.4mm 1.8mm |
L15 W15 | 1.6mm 4.8mm |
A | 0.25mm 1.6mm |
B | 1mm 1.75mm |
C | 0.8mm 4.8mm |
D | 2mm 0.5mm |
E | 2mm 0.5mm |
F | 2mm 0.5mm |
G | 2mm 0.5mm |
H | 2mm 0.5mm |
P | 45 |
Equation (1) describes the simplest case of unequal power division. The impedance is varied at the output ports because of the different widths of the feed at the output ports. The relation between the impedance at ports and the amount of power division is described in equations (2) and (3). Equations (4) to (7) describe the unequal power division and its relation to impedance. Given that port 1 is matched, the formula for calculating the input time average power is P=V/Z, where V is the junction’s phasor (total) voltage. Since both ports are assumed to be matched, the output powers can be computed similarly and are given in equations (2) and (3). To achieve the desired distribution of incident power between the two output ports, the characteristic impedances of the two transmission lines are modified. The modified values of characteristic impedances are given in equations (6) and (7). The modified characteristic impedances result in unequal power division, and the ratio of unequal power division is given in equations (4) and (5). If output power is known, the impedance of the T-junction output ports can be determined. Using the above equations, the quarter wave transformer transforms impedance in order to perform power division and determine the physical dimensions of the proposed feed structure [20].
The proposed 1*8 element planar array is constructed using this feed structure and the single element circularly polarized patch antenna array as depicted in Fig. 2. and the optimal physical dimensions of the proposed antenna are given in Table 1.
The unequal power distribution to the individual patch elements is proportional to the 0.5:1:2:2:2:2:1:0.5 amplitude tapering ratio. The power divider at the T-junction is designed for this amplitude tapering ratio. The material chosen for antenna construction is 0.78 mm thick RT Duroid 5880. This substrate material’s permittivity measures 2.2. For the construction of the proposed 1*8 element planar antenna array, the circularly polarized single element antenna and the proposed feed structure are combined. This proposed antenna is mounted conformally to the vehicle’s roof, as depicted in Figs. 3 and 4, shown below.
The conformal placement of the proposed antenna reduces its visibility to human eyes and improves its mechanical properties, such as the reduction of aerodynamic drag. The rise in the number of antennas mounted on civilian vehicles makes the conformal antenna an attractive option for vehicle manufacturers.
Simulating the proposed antenna utilizes both the HFSS and CST suite tools. The reflection coefficient versus frequency graph is depicted in Fig. 5. The impedance bandwidth at -10 dB is measured using this graph, which is the industry standard. At a resonant frequency of 11.2 GHz, simulation results indicate an impedance bandwidth of 410 MHz, or 3.66% of the resonant frequency. The axial ratio of practically circularly polarized antennas should be less than 3. The axial ratio versus frequency graph is depicted in Fig. 6. This graph is used to evaluate the bandwidth of the axial ratio at 3 dB. Simulated results reveal an axial ratio bandwidth of 150 MHz at a resonant frequency of 11.2 GHz, which is 1.34% of the resonant frequency.
Figure 7 shown below depicts the linear gain versus theta relationship. The graph displays a maximum gain of 14 dB, and the difference in gain between co-polarization and cross-polarization is consistently greater than 15 dB. Figure 8 depicts the polar gain versus theta plot. Maximum gain is 13.54 dB, and the difference between co-polarization and cross-polarization gain is greater than 15 dB throughout the entire plot. Figure 9 illustrates the 3D gain versus frequency graph. The graph displays a maximum gain of 15.71 dB.
Simulating the proposed antenna utilizes both the HFSS and CST suite tools. Figure 10 depicts a reflection coefficient versus frequency graph. The impedance bandwidth at -10 dB is measured using this graph, which is the industry standard. At the resonant frequency of 11.2 GHz, simulation results indicate an impedance bandwidth of 180 MHz, or 1.6% of the resonant frequency. The axial ratio of practically circularly polarized antennas should be less than 3. The axial ratio versus frequency graph is depicted in Fig. 11. This graph is utilized to assess the axial ratio bandwidth at 3 dB. Simulated results reveal an axial ratio bandwidth of 180 MHz at a resonant frequency of 11.2 GHz, which is 1.6% of the resonant frequency. Figure 12 depicts the graph of 3D gain versus frequency. The graph indicates a peak gain of 14.39 dB.
Figures 13 and 14 depict the far field directivity versus theta plot of the circularly polarized planar array with the existing feed and the proposed feed, respectively. The results demonstrate that the proposed feed’s side lobe levels are 8.9 dB lower than the corporate feed.
Figure 15 depicts the developed planar and conformal circularly polarized microstrip array antenna with a single element. These antennas were evaluated by measuring the various parameters of radiation characteristics using a test setup comprised of a transmitting Verdant JR12 horn antenna, Vector Network Analyzer, and anechoic chamber. Figure 16 depicts the proposed antenna placed in the anechoic chamber for testing. The proposed antenna was measured with the transmitting Verdant JR12 horn antenna positioned at 2 metres distance apart. Figures 17, 18 and 19 depict simulation versus comparison plots for the various radiation characteristic parameters.
Parameter | Single Element Antenna | Proposed Planar Array | Proposed Conformal Array |
---|---|---|---|
Impedance Bandwidth (MHz) | 490 | 400 | 170 |
Axial Ratio Bandwidth (MHz) | 170 | 140 | 160 |
Gain (dB) | 5.6 | 14 | 13.33 |
Ref. | Resonant Frequency (GHz) | Gain (dBi) | Side Lobe Levels (dB) |
---|---|---|---|
[19] | 11.2 | 5.6 | 14.9 |
[21] | 13 | 19.4 | 16 |
[22] | 12.2 | 25.3 | 26.5 |
[23] | 4.3-7.4 | 5-6.5 | around 15 |
[24] | 9.3 | 11.39 | 20 |
[25] | 9.37 | 28 | 25 |
This work | 11.2 | 14.335 | 15.5 |
The proposed conformal microstrip antenna array is compared with similar antennas in recent research and is shown in Table 3 given above. At the resonant frequency, Figs. 18, 19, and 20 demonstrate good agreement between the simulated and measured values. Although the gain could not be measured directly using the test setup, it was calculated using the Friss transmission formula. Comparing the measured gain to the gain obtained through simulation, connector losses caused a slight decrease in gain. Table 2 provides a comparison between the measured radiation characteristic parameters of single element antenna, proposed planar array and proposed conformal array.
The proposed microstrip conformal circularly polarized antenna array has been designed, simulated, developed, tested, and measured for vehicular applications. RT 5880 material with a thickness of 0.78 mm was utilized as the substrate. The characteristics of the radiation were analyzed using both simulated and measured data. The proposed feed structure reduces side lobe levels by 8.9 dB compared to the current feed structure. The measured results reveal 1 dB reduction in gain when compared to the simulation findings; however, the measured values are consistent with the simulation findings. According to the measured data, the proposed antenna has a gain of 13.33 dB, an impedance bandwidth of 1.6%, and an axial ratio bandwidth of 1.6%. The proposed antenna’s enhanced axial ratio bandwidth and reduced side lobe levels make it the optimal low-profile antenna for vehicular SATCOM applications.
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Ebenezer Abishek is an Associate Professor at Vel Tech Multi Tech. Dr. Rangarajan Dr. Sakunthala Engineering College, Chennai. His research interests include antennas and electromagnetism.. He has ten years’ teaching and 7 years’ research experience. His ORCID is 0000-0003-2908-7069.
S. Ramesh is a Professor with 19 years’ teaching experience at SRM Valliammai Engineering College in Chennai. He is a senior member of the IEEE Antennas & Propagation Society (S’10-M’17-SM’18) His research interests include antennas, propagation. His ORCID is 0000-0002-2946-5296.
Parthasarathy Ramanujam is an Assistant Professor at the National Institute of Technology, Tiruchirappalli. His research interests include microwave components and circuits His ORCID is 0000-0003-3179-0036.
E. Manikandan is a Senior Assistant Professor at the Centre for Innovation and Product Development and School of Electronics Engineering at Vellore Institute of Technology, Chennai. His research interests include antennas, micromachining and sensors. His ORCID is 0000-0002-0381-6406.
ACES JOURNAL, Vol. 38, No. 6, 439–447
doi: 10.13052/2023.ACES.J.380608
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