Gain Limits of Phase Compensated Conformal Antenna Arrays on Non-Conducting Spherical Surfaces Using the Projection Method

Gain Limits of Phase Compensated Conformal Antenna Arrays on Non-Conducting Spherical Surfaces Using the Projection Method

WiSEE 2013 1569798205 Gain Limits of Phase Compensated Conformal Antenna Arrays on Non-Conducting Spherical Surfaces using the Projection Method Bilal Ijaz, Alarka Sanyal, Alfonso Mendoza-Radal, Neil F. Chamberlain Dimitris E. Anagnostou Sayan Roy, Irfan Ullah, Michael T. Reich, Jet Propulsion Laboratory (JPL) Department of Electrical Debasis Dawn and Benjamin D. Braaten California Institute of Technology and Computer Engineering Department of Electrical and Computer Engineering Pasadena, CA, USA 91109. South Dakota School of North Dakota State University Mines and Technology, Fargo, ND, USA 58102 Rapid City, SD USA 57701 Email: [email protected] Abstract—Previously, it has been shown that the projection method can be used as an effective tool to compute the ap- propriate phase compensation of a conformal antenna array on a spherical surface. In this paper, the projection method is used to study the gain limitations of a phase-compensated six- element conformal microstrip antenna array on non-conducting spherical surfaces. As a metric for comparison, the computed gain of the phase-compensated conformal array is compared to the gain of a six-element reference antenna on a flat surface with the same inter-element spacing and operating frequency. To validate these computations, a conformal phased-array antenna consisting of six individual microstrip patches, voltage controlled Fig. 1. Array on a conformal surface. phase shifters and a power divider was assembled and tested at 2.22 GHz. Overall, it is shown how much less the gain of the phase-compensated antenna is than the reference antenna for various radius values of the sphere. Index Terms—conformal antenna array, phase compensation. I. INTRODUCTION Conformal antenna arrays are used extensively in a wide variety of applications such as antennas on an aircraft [1], satellite arrays [2] and wearable networks [3]-[4]. One of the main advantages of a conformal antenna is the ability to place them on curved surfaces. This can be very useful because Fig. 2. Conformal antenna illustration of the projection method on a spherical this removes the requirement of defining a flat surface, which surface. may not be practical in some designs. On the other hand, these curved surfaces may be subjected to forces, such as vibrations, that alter the shape of the conformal surface (as above the sphere. The reference plane is defined above the shown in Fig. 1). If the shape of the conformal surface is sphere for illustration purposes only. The antenna elements changed significantly, this can have a negative impact on the on the sphere are denoted as black dots and the elements in radiation pattern of the conformal antenna array [5]-[9]. the reference plane are denoted as grey dots. One application Fortunately, various methods have been proposed to improve of the projection method is to project the elements on the the radiation pattern of a conformal array on a changing sur- sphere onto the reference plane and consider the radiation face [10]-[19]. Among these methods is the projection method from the projected array. This consideration assumes that the [20]. For illustration of the projection method, consider the desired radiation of the array on the sphere is in the z-direction conformal antenna on the curved surface in Fig. 2. This and that appropriate phase compensation has been utilized to problem consists of six antenna elements placed on a cross- ensure that the radiated field from each antenna element on section of a sphere with radius r. A reference plane is also the sphere arrives at the reference plane with the same phase. defined to be orthogonal to the z-axis (i.e., in the x-y plane) This will ensure a broadside radiation to the reference plane. 1 element on the sphere, dproj,1 = dproj,2 = dproj,3. Therefore, the projected array should be considered as an array with a zero inter-element phase shift and a non-uniform spacing. To compute the gain from the array with non-uniform spacing, the following gain expression reported in [22] was used: 2 N−1 A Fig. 3. (a) 1 × 6 fabricated array mounted on a flat surface and (b) layout k=0 k of each individual patch (w = 48.0 mm, h = 39.64 mm, g = 2.0 mm and y = G = (3) N−1 N−1 j(α −α ) sin[β(xm−xp)] 11.0 mm). AmApe m p m=0 p=0 β(xm−xp) th where xn is the location of the n element projected onto th The objective of this work is to use the projection method the reference plane, An is the amplitude of the n element, to study the gain limitations of a phase-compensated array on αm = αn due to phase compensation and ideal elements were the non-conducting spherical surface in Fig. 2. The specific assumed. array considered for this work is the six-element conformal For comparison purposes, a six element reference array on a array shown in Fig. 3 (on a flat surface) with a spacing of flat surface (i.e., r = ∞) with a spacing of λ/2 will be defined. λ/2 at an operating frequency of 2.22 GHz. Then, the gain shift Gs reported in [6] will be computed in Related work of a conformal array on a wedge-shaped the following manner: surface has been conducted and reported in [21]. In particular, this work presented analytical expressions that can be used to Gs = Gc − Gr (4) compute the gain of the phase-compensated array with respect G to a flat array. The research reported in this paper differs in where c is the compensated gain in the z-direction and G G two ways. Namely, spherical surfaces are considered and the r is the gain of the flat reference antenna. c can be projected array has non-linear spacing. determined by computing the gain of the non-uniformly spaced flat projected antenna array and Gr can be computed using II. BACKGROUND the gain expressions reported in [22] for a Uniformly Excited, As mentioned above, one method of achieving radiation in Equally Spaced Linear Array (UE,ESLA). the z-direction in Fig. 2 is to have each radiated field from the antenna elements on the sphere arrive at the reference III. ANALYTICAL AND MEASUREMENT RESULTS plane with the same phase. To compute the amount of phase For measurement validation purposes, the prototype con- introduced by the propagation from the elements on the sphere formal phased-array antenna shown in Fig. 3 was developed. to the reference plane, the following equation can be used [6]: More specifically, this prototype was used to experimentally validate the phase compensation expressions in (2) and the Δφn = −kr(1 − sin φn) (1) gain shift values. The individual patch elements were designed th where φn is the angle of the n element on the sphere for a center frequency of 2.22 GHz on a Rogers RT/Duroid measured from the +y-axis. For the expression in (1), the 6002 grounded substrate [23] with a thickness of 20 mils reference plane has been moved to the top of the upper- (r =2.94, tan δ =0.0012) and the spacing between hemisphere in Fig. 2. Therefore, to cancel this negative phase adjacent elements in the array was fixed at λ/2. The six due to propagation to the reference plane, a phase shifter was individual elements of the array were connected to individual used to introduce a positive compensation phase of voltage controlled phase shifters with identical SMA cables. Then, each phase shifter was connected to a single port on Δφc = −Δφ n n (2) the power splitter. The commercially available phase shifters at the nth element. Next, the gain of the projected array were designed by Hittite Microwave Corporation (part no: (i.e. phase compensated array) needs to be computed in the HMC928LP5E) [24] on a connectorized board. broadside direction. To do this, the spacing dproj of the projected array will be computed in terms of the radius of A. Flat Surface (Reference Array) the sphere r and the angular location of the elements on the First, the prototype array was connected to the flat surface sphere φn. For notation, the projected elements in Fig. 2 will shown in Fig. 3 and the radiation pattern in the x-z plane was be labeled as a1, a2, a3, a4, a5 and a6 starting from the measured in a fully calibrated anechoic chamber. For these right. Then, the spacing between the projected elements a1 radiation pattern measurements all the antenna elements were and a2 can be computed as dproj,1 = r(cos φ1 − cos φ2), fed in phase. The measured S11 of the array is depicted in Fig. between the projected elements a2 and a3 can be computed 4 and the pattern measurements are shown in Fig. 5. A good as dproj,2 = r(cos φ2 − cos φ3) and between the projected match can be observed at 2.22 GHz. As a further validation, elements a3 and a4 can be computed as dproj,3 =2r cos φ3. the array was simulated in HFSS [25] at 2.22 GHz. These Due to symmetry, the spacing between elements on the left- results are also shown to agree with the measurements in Fig. hand side are similar. Because of the angles φn of each 5. 2 Fig. 4. Measured S11 of 1 × 6 Antenna platform TABLE I Fig. 5. Simulated and Measured Radiation Pattern in the x-z plane for the PHASE COMPENSATION 1 × 6 array on a flat surface. Surface Patch 1 Patch 2 Patch 3 Patch 4 Patch 5 Patch 6 TABLE II 177o 66o 7.5o 7.5o 66o 177o 20.32 cm GAIN SHIFT VALUES AS COMPARED TO FLAT ARRAY 27.94 cm 133o 48o 5o 5o 48o 133o Surface uncorrected corrected 20.32 cm -11.5 dBi -2 dBi 27.94 cm -6.5 dBi -2 dBi B.

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