15. 16. 17. 18. 19. 20. tions times de 3-D Green’s function or its gradient on a plane triangle, IEEE Trans Antennas Propagat 41 (1993), 1448-1455. T.F. Eibert and V. Hansen, On the calculation of potential integrals for linear source distributions on triangular domains, IEEE Trans Antennas Propagat 43 (1995), 1499-1502. M.G. Duffy, Quadrature over a pyramid or cube of integrands with a singularity at a vertex, SIAM J Numer Anal 19 (1982), 1260-1262. L. Rossi and P.J. Cullen, On the fully numerical evaluation of the linear-shape function times the 3-D Green’s function on a plane triangle, IEEE Trans Microwave Theory Tech 47 (1999), 398-402. M.A. Khayat and D.R. Wilton, Numerical evaluation of singular and near-singular potential integrals, IEEE Trans Antennas Propag 53 (2005). A.R. Krommer and C.W. Ueberhuber, Computational integration, Society for Industrial and Applied Mathematics, Philadelphia, PA, 1998. W.-H. Tang and S.D. Gedney, An efficient evaluation of near singular surface integrals via the Khayat-Wilton transform, Microwave Opt Technol Lett 48 (2006). © 2007 Wiley Periodicals, Inc. CAD FORMULAS FOR PATCH DIMENSIONS OF RECTANGULAR MICROSTRIP ANTENNAS WITH VARIOUS SUBSTRATE THICKNESSES Ali Akdagli Faculty of Engineering, Department of Electrical and Electronics Engineering, Mersin University, 33343 Ciftlikkoy, Mersin, Turkey means that the patch length is approximately one-half of the wavelength in the substrate material. Besides, the patch length affects the resonant resistance and the E-plane radiation pattern. The patch width affects the resonant frequency, the efficiency, the bandwidth, the H-plane radiation pattern, and the cross polarization. To select the patch width properly, it must be considered that, due to the excitation of surface waves, a small width results in a large bandwidth, and low antenna efficiency and gain. However, a large width results in the excitation of high-order modes, which may distort the radiation pattern, decrease the bandwidth, and increase the efficiency. To avoid exciting higher order modes, the patch width must be less than a wavelength in the substrate [18]. Several formulas varying in computation effort and accuracy for calculating the physical dimensions of rectangular MSAs are available in the literature [1–17, 22]. However, they do not achieve similar results, and the patch dimensions computed by using most of these formulas do not agree well with the measured data. The rectangular MSA designer needs the simple and accurate formulas to calculate the physical dimensions. In this letter, therefore, the simple and accurate formulas for computing the patch length and patch width are successfully developed by utilizing a differential evolution [23]. The differential evolution is a simple, fast, and robust evolutionary algorithm that has proven effective in determining the global optimum for general type of numeric optimization problems. It does not require initial guesses, does not use derivatives, and, it is also independent of the complexity of the objective function considered. Since its introduction, differential evolution has been rapidly gaining in acceptance, and has already been applied to the solution of various challenging engineering tasks [24 –27]. Received 5 February 2007 ABSTRACT: This letter presents the closed-from formulas for determining the patch dimensions of electrically thin and thick rectangular microstrip antennas. The presented formulas constructed by utilizing a differential evolution algorithm become very useful as computer-aided design (CAD) models for patch antenna design. A comparison between the calculated and experimental results derived from 33 patch antennas demonstrates that the proposed CAD formulas provide ⬍0.16% and 0.22% errors on average for the patch length and patch width, respectively. The results obtained by using the formulas given here are found to be closer to the experimental values, as compared with previous results presented by several researchers. © 2007 Wiley Periodicals, Inc. Microwave Opt Technol Lett 49: 2197–2201, 2007; Published online in Wiley InterScience (www.interscience.wiley.com). DOI 10.1002/mop. 22679 2. PATCH DIMENSIONS OF RECTANGULAR MICROSTRIP ANTENNAS Figure 1 shows a typical rectangular MSA consisting of a patch of length L and width W over a ground plane with a substrate of thickness h and a relative dielectric constant r. When a rectangular MSA design is concerned, a proper dielectric substrate material is firstly selected, and then the values of patch length and patch Key words: rectangular microstrip antennas; patch dimensions; differential evolution; CAD 1. INTRODUCTION Microstrip antennas (MSAs) are becoming a popular choice for a broad range of applications from portable wireless communication systems to biomedical systems [1–10]. Although they have some advantages, such as light weight, low profile, low cost, easy manufacturing, high level of integration, the possibility of making conformal antennas, they also have some disadvantages, such as narrow bandwidth, low overall efficiency due to dielectric losses, and the generation of surface waves at the air dielectric interface. A rectangular patch antenna is the most widely used MSA, and is characterized by its length and width [1–22]. The proper selection of patch dimensions of rectangular MSAs is important in the design, because the antenna performance characteristics depend firmly on the physical dimensions. For instance, the rectangular MSA radiates efficiently when it resonates, which DOI 10.1002/mop Figure 1 Geometry of a rectangular MSA MICROWAVE AND OPTICAL TECHNOLOGY LETTERS / Vol. 49, No. 9, September 2007 2197 TABLE 1 Comparison of Measured and Computed Patch Lengths of Rectangular Microstrip Antennas L (cm) ⑀I h (cm) (h/d) fI (MHz) Measured [16, 7] 2.22 2.22 2.22 2.55 10.2 2.33 2.33 2.55 2.55 2.55 2.55 2.55 2.50 2.50 2.50 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 0.017 0.017 0.079 0.079 0.127 0.157 0.157 0.163 0.163 0.200 0.242 0.252 0.300 0.300 0.300 0.476 0.330 0.400 0.450 0.476 0.476 0.550 0.626 0.854 0.952 0.952 0.952 1.000 1.100 1.200 1.281 1.281 1.281 0.006535 0.007134 0.015577 0.032505 0.062193 0.040421 0.038384 0.056917 0.048587 0.066004 0.090814 0.077800 0.083326 0.126333 0.103881 0.129219 0.140525 0.151895 0.145395 0.147462 0.16165 0.175363 0.155278 0.209105 0.181413 0.201683 0.197629 0.211852 0.228353 0.221646 0.218197 0.203196 0.214787 7740 8450 3970 7730 4600 5060 4805 6560 5600 6200 7050 5800 5270 7990 6570 5100 8000 7134 6070 5820 6380 5990 4660 4600 3580 3980 3900 3980 3900 3470 3200 2980 3150 1.290 1.185 2.500 1.183 1.000 1.860 1.960 1.350 1.621 1.412 1.200 1.485 1.630 1.018 1.280 1.580 1.080 1.255 1.450 1.520 1.440 1.620 1.970 2.300 2.756 2.620 2.640 2.676 2.835 3.130 3.380 3.500 3.400 This letter Eq. (5) Eq. (7) [7] [12] [1, 6, 15] [16, 7] [22] 1.294 1.185 2.500 1.179 1.000 1.862 1.966 1.349 1.596 1.411 1.202 1.486 1.639 1.021 1.280 1.579 1.080 1.261 1.448 1.521 1.457 1.619 1.953 2.301 2.756 2.612 2.640 2.676 2.835 3.139 3.377 3.502 3.404 1.290 1.185 2.500 1.182 1.000 1.862 1.960 1.346 1.599 1.413 1.199 1.489 1.632 1.017 1.281 1.580 1.080 1.257 1.446 1.522 1.455 1.620 1.955 2.298 2.756 2.620 2.640 2.680 2.834 3.130 3.381 3.500 3.400 1.300 1.190 2.512 1.184 0.987 1.867 1.971 1.349 1.599 1.407 1.189 1.477 1.625 0.992 1.258 1.534 0.960 1.054 1.254 1.303 1.158 1.199 1.603 1.452 1.982 1.706 1.757 1.668 1.637 1.871 2.045 2.272 2.094 1.275 1.168 2.485 1.191 1.001 1.903 2.004 1.403 1.644 1.485 1.306 1.587 1.764 1.164 1.415 1.805 1.151 1.290 1.517 1.582 1.443 1.537 1.975 2.001 2.571 2.313 2.360 2.313 2.360 2.653 2.877 3.089 2.922 1.299 1.189 2.508 1.183 1.010 1.864 1.968 1.351 1.600 1.412 1.200 1.485 1.636 1.107 1.275 1.577 0.997 1.109 1.309 1.365 1.232 1.300 1.691 1.672 2.169 1.933 1.976 1.932 1.970 2.217 2.404 2.585 2.442 1.298 1.189 2.508 1.183 1.009 1.864 1.968 1.351 1.600 1.412 1.200 1.485 1.636 1.016 1.275 1.577 1.085 1.264 1.454 1.527 1.459 1.618 1.957 2.301 2.754 2.612 2.638 2.677 2.836 3.140 3.379 3.501 3.405 1.291 1.182 2.502 1.181 1.002 1.865 1.969 1.350 1.598 1.411 1.202 1.486 1.639 1.020 1.279 1.577 1.080 1.262 1.449 1.523 1.458 1.619 1.955 2.301 2.756 2.613 2.640 2.676 2.831 3.137 3.376 3.502 3.404 width are determined for a given operating frequency. It is clear from all of the formulas presented in the literature [1–17, 22] that only three parameters, h, r, and resonant frequency fr, are required to describe the patch dimensions of rectangular MSAs. However, it is difficult to accurately determine the patch dimensions, because MSA is inhomogeneous and the radiation appears at the edges of the patch. Many of the formulas available do not provide a ready solution for finding the patch dimensions of a rectangular MSA for a given operating frequency. The latest formulas proposed by Guney [22] for computing the patch dimensions of the rectangular MSAs with thin and thick substrates are given as 冦 冦 0.51 d共h/d兲0.0112 ⫺ 0.565h共h/d兲⫺0.117 ⫹ 0.014o, if h/d ⱕ 0.13 L ⫽ 383.0445 共h/ 兲0.00052 ⫹ 0.36h共h/ 兲0.014 ⫺ 239.37 , (1) d d d o if h/d ⬎ 0.13 9.8636 d共h/d兲0.4561 ⫺ 10.9h共h/d兲⫺0.446 ⫹ 0.00204o, if h/d ⱕ 0.13 W ⫽ 382.466 共h/ 兲⫺0.000907 ⫺ 0.0003h共h/ 兲⫺0.04 ⫺ 239.73 , d d d o if h/d ⬎ 0.13 (2) with 2198 d ⫽ o 冑r ⫽ c fr 冑r (3) where d is the wavelength in the dielectric substrate, o is the free-space wavelength, and c is the velocity of electromagnetic waves in free space. In this letter, based on the experimental data available in the literature [16, 17], the simple and accurate CAD models are provided for calculating the patch length and patch width of the rectangular MSAs with thin and thick substrates. To find proper models for the patch dimensions, several experiments were carried out. The coefficient values of the models found are then optimally determined by utilizing differential evolution so as to minimize the following total absolute errors (TAE) TAE ⫽ ⌺兩PDme ⫺ PDca兩 (4) where PDme and PDca are, respectively, the measured and calculated patch dimension (L or W). Two methods given as follows are proposed for the calculation of patch dimensions. MICROWAVE AND OPTICAL TECHNOLOGY LETTERS / Vol. 49, No. 9, September 2007 DOI 10.1002/mop TABLE 2 Comparison of Measured and Computed Patch Widths of Rectangular Microstrip Antennas L (cm) ⑀I h (cm) (h/d) fI (MHz) Measured [16, 7] 2.22 2.22 2.22 2.55 10.2 2.33 2.33 2.55 2.55 2.55 2.55 2.55 2.50 2.50 2.50 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 2.55 0.017 0.017 0.079 0.079 0.127 0.157 0.157 0.163 0.163 0.200 0.242 0.252 0.300 0.300 0.300 0.476 0.330 0.400 0.450 0.476 0.476 0.550 0.626 0.854 0.952 0.952 0.952 1.000 1.100 1.200 1.281 1.281 1.281 0.006535 0.007134 0.015577 0.032505 0.062193 0.040421 0.038384 0.056917 0.048587 0.066004 0.090814 0.077800 0.083326 0.126333 0.103881 0.129219 0.140525 0.151895 0.145395 0.147462 0.16165 0.175363 0.155278 0.209105 0.181413 0.201683 0.197629 0.211852 0.228353 0.221646 0.218197 0.203196 0.214787 7740 8450 3970 7730 4600 5060 4805 6560 5600 6200 7050 5800 5270 7990 6570 5100 8000 7134 6070 5820 6380 5990 4660 4600 3580 3980 3900 3980 3900 3470 3200 2980 3150 0.850 0.790 2.000 1.063 0.910 1.720 1.810 1.270 1.500 1.337 1.120 1.403 1.530 0.905 1.170 1.375 0.776 0.790 0.987 1.000 0.814 0.790 1.200 0.783 1.256 0.974 1.020 0.883 0.777 0.920 1.030 1.265 1.080 This letter Eq. (6) Eq. (8) [13] [14] [1, 11, 15] [16, 7] [22] 0.850 0.795 2.000 1.063 0.903 1.723 1.810 1.272 1.495 1.334 1.119 1.399 1.538 0.896 1.171 1.375 0.776 0.790 0.980 1.004 0.818 0.786 1.177 0.782 1.256 0.963 1.016 0.881 0.763 0.920 1.032 1.270 1.084 0.850 0.790 2.000 1.065 0.908 1.719 1.810 1.271 1.498 1.337 1.120 1.405 1.535 0.901 1.169 1.379 0.776 0.790 0.981 1.001 0.828 0.784 1.190 0.782 1.256 0.974 1.020 0.879 0.776 0.920 1.031 1.261 1.080 1.163 1.065 2.267 1.164 1.957 1.779 1.873 1.372 1.607 1.452 1.277 1.552 1.708 1.126 1.370 1.765 1.125 1.262 1.483 1.546 1.411 1.503 1.931 1.957 2.514 2.261 2.308 2.261 2.308 2.594 2.813 3.020 2.857 2.341 2.145 4.565 2.187 1.838 3.496 3.681 2.577 3.019 2.727 2.398 2.915 3.240 2.137 2.599 3.315 2.114 2.370 2.786 2.905 2.650 2.823 3.628 3.676 4.723 4.248 4.335 4.248 4.335 4.873 5.284 5.674 5.368 1.527 1.399 2.978 1.457 1.378 2.297 2.419 1.716 2.010 1.816 1.597 1.941 2.152 1.419 1.726 2.208 1.407 1.578 1.855 1.935 1.765 1.880 2.416 2.448 3.145 2.829 2.887 2.829 2.887 3.245 3.518 3.778 3.574 0.848 0.794 2.001 1.063 0.905 1.725 1.811 1.275 1.497 1.337 1.123 1.404 1.153 0.902 1.177 1.385 0.777 0.798 0.987 1.013 0.828 0.793 1.192 0.783 1.265 0.964 1.018 0.884 0.777 0.929 1.039 1.271 1.088 0.848 0.794 2.000 1.062 0.910 1.722 1.808 1.273 1.495 1.335 1.120 1.400 1.539 0.897 1.172 1.377 0.773 0.796 0.982 1.009 0.826 0.791 1.187 0.780 1.262 0.961 1.015 0.881 0.773 0.925 1.035 1.267 1.084 The First Method W 冦 0.483 d ⫺ 0.5957h ⫹ 0.0281ocos共共h/d兲⫺0.02142 兲, if h/d ⱕ 0.13 (5) L ⫽ 0.265 ⫹ 1.4097h ⫹ 0.0029 cos共共h/ 兲⫺1.099 兲, d o d if h/d ⬎ 0.13 冦 0.5913 d ⫺ 2h ⫹ 0.3211dcos共共h/d兲⫺0.1798 兲, if h/d ⱕ 0.13 W ⫽ 1.2848 ⫺ 3.636h ⫹ 0.4469 cos共共h/ 兲⫺0.5626 兲, (6) d d d if h/d ⬎ 0.13 冦 0.5909d ⫺ 2h ⫹ 0.3241dcos共共h/d兲⫺0.179 兲 ⫹ 0.0009ocos共共h/d兲⫺1.75565 兲, if h/d ⱕ 0.13 ⫽ 0.5811 ⫺ 1.83h ⫺ 0.0092 cos共共h/ 兲⫺1.0825 兲 d d d ⫺ 0.0013ocos共共h/d兲⫺3.1727 兲, if h/d ⬎ 0.13 (8) The formulas for calculation of patch dimensions suggested in the first method are simpler than those suggested in the second method, however, the formulas of the second method achieve more accurate results. Thus, the antenna designer can make a trade-off between the simplicity and the accuracy. 3. RESULTS AND CONCLUSIONS The Second Method L 冦 0.4826 d ⫺ 0.6115h ⫹ 0.0015dcos共共h/d兲⫺1.9133 兲 ⫹ 0.0305ocos共共h/d兲⫺0.0275 兲, ⫽ 0.2716 ⫹ 1.3711h ⫹ 0.0063 cos共共h/ 兲⫺1.1116 兲 d d d ⫺ 0.00065ocos共共h/d兲⫺3.7 兲, if h/d ⱕ 0.13 if h/d ⬎ 0.13 (7) DOI 10.1002/mop To appraise the validity and accuracy of the new formulas suggested for patch dimensions, the calculations were carried out on 33 rectangular patch antennas built on various substrates. The antennas, which consist in measurement data [16, 17] given in Tables 1 and 2, vary in electrical thickness, defined as h/d, from 0.006535 to 0.228353, and in physical thickness from 0.017 to 1.281 cm, and operate over the frequency range 2980 – 8450 MHz. The results calculated by using the formulas given in the first and second methods for the patch length L and patch MICROWAVE AND OPTICAL TECHNOLOGY LETTERS / Vol. 49, No. 9, September 2007 2199 TABLE 3 Total Absolute Errors Between the Measured and Computed Patch Lengths (L) can be very useful for many engineering applications because of their simplicity and high accuracy. This letter Eq. (5) Eq. (7) [7] [12] [1, 6, 15] [16, 7] [22] REFERENCES (TAE) (cm) 0.130 0.085 12.762 5.244 9.349 0.170 0.140 TABLE 4 Total Absolute Errors Between the Measured and Computed Patch Widths (W) This letter Eq. (6) Eq. (8) (TAE) (cm) 0.133 0.072 [13] [14] 22.553 74.122 [1, 11, 15] [16, 7] 36.918 0.164 [22] 0.143 width W are, respectively, tabulated in Tables 1 and 2. To make a comparison, these tables also contain the patch dimensions measured [16, 17] and those computed by other scientists [1, 6, 7, 11–17, 22]. Total absolute errors between the measured and calculated by every suggestion for the patch length and patch width are listed in Tables 3 and 4, respectively. As it can be seen from Tables 1 and 2, the methods previously published in the literature for the patch dimensions give comparable results—some cases are in good agreement with measured data, and others are far off. From the Tables 3 and 4, the patch dimensions obtained by using the formulas given in the first method and the second method proposed in this work provide the more accurate results, as compared with those reported by the other researchers. The formulas given by Eqs. (7) and (8) in the second method achieve the best results, and the average percentage deviations for the patch length and patch width are found to be 0.16% and 0.22%, respectively, for 33 rectangular MSAs considered in this work. The results reported by Kara [16, 17] and Guney [22] are also close to the experimental results, however, the proposed formulas given by Eqs. (5) and (6) in the first method not only are simpler and but provide the more accurate results. The better agreement between the measured and our computed patch dimension results supports the validity and accuracy of the new formulas. The formulas proposed here are suitable for CAD and are directly applicable for the integration of rectangular MSAs. These CAD formulas are very useful to antenna engineers since they require no complicated mathematical functions and no iterative techniques. By using a hand calculator, one can accurately compute the patch dimensions without possessing any background knowledge of the rectangular MSAs. 4. CONCLUSION In this letter, the simple and accurate CAD formulas for the calculation of patch length and width of the rectangular MSAs with various substrate thicknesses, which can be readily used by a MSA designer practically without any background in sophisticated mathematical techniques, are presented. They are obtained by utilizing the differential evolution algorithm. Two methods for the patch dimension formulation, which give a trade-off between the simplicity and the accuracy, are suggested. The validity of the new formulas has been verified by comparing the achieved patch dimension results with the experimental results. The CAD formulas proposed in this work 2200 1. I.J. Bahl and P. Bhartia, Microstrip antennas, Artech House, Dedham, MA, 1980. 2. J.R. James, P.S. Hall, and C. Wood, Microstrip antennas-theory and design, Peter Peregrinus, London, 1981. 3. J.R. Mosig and F.E. Gardiol, A dynamic radiation model for microstrip structures, In: Advances in electronics and electron physics, Vol. 59, Academic Press, New York, 1982, pp. 139 –227. 4. R.E. Munson, Microstrip antennas, In: R.C. Johnson (Ed.), Antenna engineering handbook, 3rd ed., McGraw-Hill, New York, 1983. 5. K.C. Gupta and A. Benalla (Eds.), Microstrip antenna design, Artech House, Canton, MA, 1988. 6. Y.T. Lo, S.M. Wright, and M. Davidovitz, Microstrip Antennas, In: K. Chang (Ed.), Handbook of microwave and optical components, Vol. 1, Wiley, New York, 1989, pp. 764 – 889. 7. D.M. Pozar and D.H. Schaubert (Eds.), Microstrip antennas-the analysis and design of microstrip antennas and arrays, IEEE Press, New York, 1995. 8. R.A. Sainati, CAD of microstrip antennas for wireless applications, Artech House, Norwood, MA, 1996. 9. K.F. Lee and W. Chen, Advances in microstrip and printed antennas, Wiley, New York, 1997. 10. R. Garg, P. Bhartia, I. Bahl, and A. 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Guney, Simple and accurate formulas for the physical dimensions of rectangular microstrip antennas with thin and thick substrates, Microwave Opt Technol Lett 44 (2005), 257–259. 23. R. Storn and K. Price, Differential evolution—A simple and efficient heuristic for global optimization over continuous spaces, J Global Optimizat 11 (1997), 341–359. 24. K.A. Michalski, Electromagnetic imaging of elliptical cylindrical conductors and tunnels using a differential evolution algorithm, Microwave Opt Technol Lett 28 (2001), 164 –169. 25. X.F. Luo, A. Qing, and C.K. Lee, Application of the differential- MICROWAVE AND OPTICAL TECHNOLOGY LETTERS / Vol. 49, No. 9, September 2007 DOI 10.1002/mop evolution strategy to the design of frequency-selective surfaces, Int J RF Microwave Computer Aided Eng 15 (2005), 173–180. 26. A. Akdagli and M.E. 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ANALYSIS OF ELECTROMAGNETIC BAND-GAP WAVEGUIDE STRUCTURES USING BODY-OF-REVOLUTION FINITEDIFFERENCE TIME-DOMAIN METHOD Ming-Sze Tong,1 Ronan Sauleau,2 Anthony Rolland,2 and Tae-Gyu Chang1 1 School of Electrical and Electronics Engineering, Chung-Ang University, 221 Heukseok-dong, Dongjak-gu, Seoul 156 –756, Korea 2 Institute of Electronics and Telecommunications of Rennes, University of Rennes I, Campus de Beaulieu, 263 Avenue du Général Leclerc, 35042 Rennes, France Received 12 February 2007 ABSTRACT: Study of electromagnetic band-gap (EBG) structures has become a hot topic in computational electromagnetics. In this article, some EBG structures integrated inside a circular waveguide are studied. They are formed by a series of air-gaps within a circular dielectric-filled waveguide. A body-of-revolution finite-difference time-domain (BOR-FDTD) method is adopted for analysis of such waveguide structures, due to their axial symmetric properties. The opening ends of the waveguide are treated as a matched load using an unsplit perfectly matched layer technique. Excitations on a waveguide in BOR-FDTD are demonstrated. Numerical results of various air-gap lengths with respect to the period of separation are given, showing an interesting tendency of EBG behavior. A chirpingand-tapering technique is applied on the EBG pattern to improve the overall performance. The proposed EBG structures may be applied into antenna structures or other system for unwanted signal suppression. Results show that the BOR-FDTD offers a good alternative in analyzing axial symmetric configurations, as it offers enormous savings in computational time and memory comparing with a general 3D-FDTD algorithm. © 2007 Wiley Periodicals, Inc. Microwave Opt Technol Lett 49: 2201–2206, 2007; Published online in Wiley InterScience (www.interscience.wiley.com). DOI 10.1002/mop.22668 Key words: EBG structures; circular dielectric-filled waveguide; BORFDTD method candidate in guided wave structures, since the traveling EM waves are well confined inside the dielectrically filled substrate of the device during transmission. Their axial symmetric nature ensures an even field distributions along the azimuthal () direction at a cross section. Because of the nonexistence of a secondary conducting medium other than the outer metallic shell, waveguides support generally non-TEM (transverse electromagnetic) mode operations, such as transverse electric (TE) or transverse magnetic (TM) modes. In terms of analyzing tool, a body-of-revolution finite-difference time-domain (BOR-FDTD) method is adopted for analysis [7, 8], due to the axial symmetric properties existing in circular waveguide structures. The BOR-FDTD method has been demonstrated as a robust and versatile numerical tool for solving axial symmetric problems as found in [9 –11], though they can also be solved using other frequency domain methods [12–14]. BOR-FDTD is a cylindrically based algorithm, and it expands the angular dependence using Fourier series. The computational domain is thus compressed from a three-dimensional (3-D) volume into a two-dimensional (2-D) –z plane. On the other hand, an unsplit perfectly matched layer (U-PML) technique [15] is used to model the two end-walls of the waveguide as a matched load. In this article, some EBG structures integrated inside circular waveguides are taken for studies. They are constructed by aligning a series of periodic air-gaps longitudinally inside a dielectrically filled circular waveguide. Two operational modes, viz., TE11 and TM01, are used for excitations. Frequency characteristics in terms of scattering parameters are extracted for analysis. It is observed that the given EBG structures exhibit a good band-gap behavior. Additionally, to further improve the performance of bandwidth in stop-band and the low frequency side-lobes, a chirping-and-tapering technique [16] is applied on the EBG air-gap pattern. 2. THEORY 2.1. BOR-FDTD Method Derivation of BOR-FDTD starts with the general time-dependent Maxwell’s curl equations: ជ ⫽ 0关 r兴⭸Eជ /⭸t ⫹ 关e兴Eជ ⵜ⫻H ជ /⭸t ⫺ 关m 兴H ជ and ⵜ ⫻ Eជ ⫽ ⫺ 0 关r兴⭸H (1) This assumes linear and anisotropic media inside the computational domain; where [r], [r], [e], [h] are the diagonal tensors of the relative permittivity, relative permeability, electric conductivity, and magnetic conductivity, respectively. The Maxwell’s equations are expanded in cylindrical coordinates to handle cylindrical structures more efficiently. For axial symmetric structures, viz., BOR structures, the electric and magnetic fields can be expanded using infinite Fourier series [17]: 1. INTRODUCTION One of the interesting areas that have recently been broadly conducted in computational electromagnetics (CEM) is the study of electromagnetic band-gap (EBG) structures. Typically, an EBG material acts as a band-stop filtering device to suppress electromagnetic (EM) waves inside a certain frequency range. This is conventionally done through a periodic pattern of distributed elements. The concept originated in optics [1, 2], and thereafter successfully transformed into microwave areas by proper frequency downscaling (e.g. [3, 4]). Circular waveguides have been commonly used in microwave engineering due to their high power capability and low power loss during transmission [5, 6]. Dielectric waveguide is deemed as a good DOI 10.1002/mop 冘 ⬁ Eជ 共 , ,z;t兲 ⫽ 关Eជ 共 ,z;t兲 evencos共m兲 ⫹ Eជ 共,z;t兲oddsin共m兲兴 (2a) m⫽0 冘 ⬁ ជ 共,,z;t兲 ⫽ H ជ 共,z;t兲oddsin共m兲兴 ជ 共,z;t兲evencos共m兲 ⫹ H 关H (2b) m⫽0 where m is the mode number in the -direction, and the field terms with subscripts even and odd are the coefficients of cos(m) and sin(m), respectively. Solutions for Maxwell’s curl equations are obtainable by a proper selection of angular field variations, e.g., MICROWAVE AND OPTICAL TECHNOLOGY LETTERS / Vol. 49, No. 9, September 2007 2201