
- •Reconfigurable Antennas
- •ABSTRACT
- •Keywords
- •Contents
- •1.1 WHAT CONSTITUTES RECONFIGURABILITY?
- •1.2 WHY WOULD ANTENNA RECONFIGURABILITY BE USEFUL?
- •2.1 FREQUENCY RESPONSE
- •2.2 RADIATION CHARACTERISTICS
- •4.1 FUNDAMENTAL THEORY OF OPERATION
- •4.2 RECONFIGURATION MECHANISMS
- •4.2.1 Switches
- •4.2.2 Variable Reactive Loading
- •4.2.3 Structural/Mechanical Changes
- •4.2.4 Material Changes
- •5.1 FUNDAMENTAL THEORY OF OPERATION
- •5.2 RECONFIGURATION MECHANISMS
- •5.2.1 Switches
- •5.2.2 Material Changes
- •6.1 FUNDAMENTAL THEORY OF OPERATION
- •6.2 RECONFIGURATION MECHANISMS
- •6.2.1 Structural/Mechanical Changes
- •6.2.2 Electrical Changes
- •6.2.2.1 Parasitic Tuning
- •6.2.2.2 Array Tuning
- •6.2.3 Material Changes
- •7.1 FUNDAMENTAL THEORY OF OPERATION
- •7.2 ELECTRONIC RECONFIGURATION MECHANISMS
- •8.2 RECONFIGURATION MECHANISM IMPLEMENTATION
- •8.3 MATCHING NETWORKS
- •9.2 ECONOMIC VIABILITY OF RECONFIGURABILITY
- •9.3 EXPANDED DESIGN METHODOLOGIES
- •9.4 NEW TECHNOLOGIES FOR RECONFIGURABILITY IN EMERGING APPLICATIONS
- •References
- •Author Biography

26 Reconfigurable Antennas
6.2RECONFIGURATION MECHANISMS
6.2.1Structural/Mechanical Changes
With the reflective surface physically removed and isolated from the primary feed, reflector antennas are a natural choice for applications that require radiation pattern reconfiguration independent of frequency. Clarricoats and Zhou demonstrated an example of a radiation-reconfigurable reflector antenna by actively changing the structure of a mesh reflector [50]. In its first embodiment, the reflector contour was changed manually in certain regions, which resulted in changes in beam shape and direction [50]. Later, computer-controlled stepper motors were implemented to pull cables attached to specific points on the reflector mesh to support automatic pattern reconfiguration [51].
More recently, a similar system for satellite applications has been developed with expanded capabilities enabled by changes in the system’s subreflector rather than the main reflector [52]. Shown in Figure 6.1 [52], the subreflector is fabricated using a thin, flexible, conductive material, and its shape is changed using piezoelectric actuators attached to its back surface. A desired radiation pattern is achieved when the actuators deform the subreflector surface and produce changes in the electromagnetic field illuminating the main reflector. To minimize the number of actuators (and, hence, system complexity and weight), their positions are determined using an iterative finiteelement algorithm. This algorithm indicates where successive actuators should be placed to minimize the error between the desired and actual subreflector shape [52]. Figures 6.2 and 6.3 show the beam patterns supported by the antenna reconfiguration [52].
FIGURE 6.1: Reconfigurable subreflector system, including piezoelectric actuators and driver to deflect the surface of a Cassegrain subreflector (Washington et al. [52], ©IEEE 2002).

Methods for Achieving Radiation Pattern Reconfigurability 27
FIGURE 6.2: Radiation pattern for U.S. coverage using reflector antenna equipped with the mechanically reconfigurable subreflector (Washington et al. [52], ©IEEE 2002).
Changes in an effective reflector have also been demonstrated using reconfigurable highimpedance surfaces [53]. Here, a lattice of small resonant elements produces high-surface impedance near their resonant frequency, creating, in effect, an artificial ground plane. Changing the capacitances between resonant elements across the lattice through mechanical means creates a phase gradient that can produce a steered beam when the lattice is used as a reflector. An electrically tuned version of this structure using varactors that can deliver two-dimensional beam steering is discussed in [54].
A closely related approach has also been used to develop a reconfigurable leaky-wave antenna using mechanical tuning [55]. In this case, a horizontally polarized antenna is used to couple energy into leaky transverse electric waves on a tunable impedance surface. A diagram of the surface, including the moveable top capacitance surface, is shown in Figure 6.4 [55]. The radiated beam from the surface can be steered in elevation over a range of 45° by changing the apparent capacitance of the surface through mechanically shifting the top capacitive plane. The antenna and the surface are shown in Figure 6.5 [55]. An electronically tuned version of this antenna that uses varactors can produce reconfigurable backward as well as forward leaky-wave beams [56, 57].
The electromechanically scannable trough waveguide antenna, first developed in 1960, is one early example of a pattern-reconfigurable antenna [58]. Based on an asymmetrical trough waveguide intended to feed a parabolic reflector [59], two different mechanisms were proposed to alter the phase velocity in the guide that resulted in scanned radiation patterns at a single frequency. The first mechanism involved the rotation of artificial dielectric structures along a longitudinal axis

28 Reconfigurable Antennas
FIGURE 6.3: Radiation pattern for Brazil coverage using reflector antenna equipped with the mechanically reconfigurable subreflector (Washington et al. [52], ©IEEE 2002).
within the trough waveguide, and the second used a mechanical variation of the height of periodic structures located on the top of the center fin of the trough waveguide [58]. Although elegant in concept, the authors acknowledged at the time that both approaches presented major mechanical issues that they resolved using “cam-and-gear” solutions that were complex and cumbersome.
Huff and Bernhard [60] began with the concept of [58] and proposed the application of more modern perturbations and streamlined actuation mechanisms to achieve beam steering at a single frequency while preserving the wide bandwidth characteristics of the original antenna. The trough waveguide’s fundamental structure is shown in Figure 6.6 [60]. In the more modern embodiment, beam steering is achieved using micromachined cantilever structures fabricated within the trough waveguide, shown in Figure 6.7 [60]. These cantilevers, which can be actuated electrostatically or magnetostatically, create perturbations that change the apparent phase velocity in the waveguide and produce scanned radiation patterns. Simulations with actuation of individual cantilevers or groups of cantilevers demonstrate beam scanning at single frequencies through broadside for this traveling wave antenna [60].

Methods for Achieving Radiation Pattern Reconfigurability 29
FIGURE 6.4: Mechanically reconfigurable impedance surface consisting of two printed circuit boards: a high-impedance ground plane and a separate tuning layer. The tuning layer is moved across the stationary high-impedance surface to vary the capacitance between the overlapping plates and tune the resonance frequency of the surface (Sievenpiper et al. [55], ©IEEE 2002).
FIGURE 6.5: A horizontally polarized antenna couples energy into leaky modes on the tunable impedance surface. The waves propagate across the surface and radiate at an angle governed by the surface resonance frequency with respect to the excitation frequency. By tuning the surface resonance frequency, the beam is steered in the elevation plane (Sievenpiper et al. [55], ©IEEE 2002).

30 Reconfigurable Antennas
FIGURE 6.6: Trough waveguide dimensions (left), electric field lines of the dominant transverse electric mode with equivalent structure for design and field distribution (middle), electric field lines of the transverse electromagnetic mode (right) (Huff and Bernhard [60], ©Huff and Bernhard 2005).
FIGURE 6.7: Trough waveguide with cantilever-type perturbations, showing staggered positions of actuated and rest states of the cantilevers (Huff and Bernhard [60], ©Huff and Bernhard 2005).
Another approach using micromachined components has also been demonstrated that uses mechanical changes in a hornlike antenna to produce reconfigurable radiation patterns with no appreciable changes in frequency response [61]. The basic antenna, shown in Figure 6.8 [61] is composed of a planar “V” structure with a coplanar transmission line feed. Micromachined rotational hinges fixed to the substrate material hold the ends of each of the “V” arms in place. MEMS actuators move the arms laterally to alter the radiated main beam direction and/or beam shape [61]. Figures 6.9 and 6.10 [61] show some of the possible beam variation achieved with this structure [61].
Chang et al. enable mechanical perturbation of propagation constants in a dielectric waveguide antenna operating at millimeter-wave frequencies to achieve pattern reconfigurability [62].

Methods for Achieving Radiation Pattern Reconfigurability 31
FIGURE 6.8: (a) Conceptual diagram and (b) cross section of a MEMS reconfigurable Vee antenna (Chiao et al. [61], ©IEEE 1999).
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FIGURE 6.9: E-plane beam-steering patterns for a 17.5-GHz 75° Vee antenna (Chiao et al. [61], ©IEEE 1999).