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LPDA Antenna Array: Design & Applications

Updated 7 February 2026
  • LPDA antenna arrays are broadband antennas comprising systematically varying dipoles that deliver scalable performance over a wide frequency range.
  • They employ geometric scaling factors and controlled apex angles to achieve optimal impedance matching, moderate gain, and minimal VSWR.
  • Practical designs are validated through full-wave simulations and in-situ calibrations, ensuring reliable performance in radio astronomy and cosmic-ray detection.

A log-periodic dipole antenna array (LPDA) is a broadband, frequency-scalable antenna realized as a sequence of half-wave dipoles of systematically varying length and spacing. Each element is mounted parallel on one or more conducting booms, with the lengths and spacings scaled by a fixed factor to achieve stable impedance, directivity, and pattern characteristics over an octave or larger frequency ratio. LPDAs are widely employed for applications ranging from radio astronomy and cosmic-ray detection to electromagnetic compatibility testing, leveraging their wideband impedance match, moderate gain, and controllable polarization properties (Briechle, 2016, Acedo et al., 2020, Seikh et al., 20 Jan 2026).

1. Geometric Parameters and Design Laws

LPDA design is governed by the log-periodic principle, wherein the n-th dipole element possesses length Ln=L1τn−1L_n=L_1\tau^{n-1} and spacing Sn=S1τn−1S_n=S_1\tau^{n-1}, with L1L_1 and S1S_1 being the largest element parameters, τ<1\tau<1 a constant scale factor, and n=1…Nn=1\ldots N (Seikh et al., 20 Jan 2026, Acedo et al., 2020). L1L_1 is typically set by the lowest design frequency (L1≈c/(2fmin)L_1\approx c/(2f_\text{min})), and NN is calculated to provide the needed bandwidth, N=1+log⁡(fmax⁡/fmin⁡)/log⁡(1/τ)N=1+\log(f_{\max}/f_{\min})/\log(1/\tau).

The apex angle Sn=S1τn−1S_n=S_1\tau^{n-1}0 regulates the mechanical spread and pattern envelope, typically set by Sn=S1τn−1S_n=S_1\tau^{n-1}1 for Sn=S1τn−1S_n=S_1\tau^{n-1}2 (Acedo et al., 2020). Typical parameters, as realized in the SKALA4 (SKA1-LOW) element, include Sn=S1τn−1S_n=S_1\tau^{n-1}3, Sn=S1τn−1S_n=S_1\tau^{n-1}4, Sn=S1τn−1S_n=S_1\tau^{n-1}5 m, Sn=S1τn−1S_n=S_1\tau^{n-1}6 m, and Sn=S1τn−1S_n=S_1\tau^{n-1}7 for 50–350 MHz performance (Acedo et al., 2020). The AERA LPDA at Pierre Auger Observatory uses Sn=S1τn−1S_n=S_1\tau^{n-1}8, Sn=S1τn−1S_n=S_1\tau^{n-1}9, and covers 30–80 MHz with element lengths from L1L_101 m to 5.3 m (Briechle, 2016). Optimal element diameter is selected for bandwidth and structural integrity, typically 10–15 mm for tubular conductors at these frequencies (Acedo et al., 2020, Seikh et al., 20 Jan 2026).

2. Impedance Matching and Feeding Structure

Consistent impedance is a signature LPDA feature. The input impedance L1L_11 is achieved using a wideband balanced/unbalanced (balun) transformer, either via coaxial sleeves (SKALA4 design) or other transmission line structures. The design aims for VSWR L1L_12 over most of the operational frequency range, with reactance kept below L1L_13 and often improved by minor capacitive tuning (L1L_14–4 pF) (Acedo et al., 2020).

Reflection coefficient L1L_15, return loss L1L_16 dB, and Smith chart loci are extracted from measured or simulated S-parameters, with a typical design goal of L1L_17 dB across the band for robust matching (Seikh et al., 20 Jan 2026). AAFIYA [Editor’s term] provides reference Python workflow for automated S-parameter extraction, impedance analysis, and publication-quality visualization, supporting validation against simulation data (Seikh et al., 20 Jan 2026).

3. Radiation Characteristics and Polarization Properties

The directional response of an LPDA is described by its vector effective length (VEL) L1L_18, which yields the open-circuit voltage L1L_19 (Briechle, 2016). The gain S1S_10 relates to the effective height S1S_11 via

S1S_12

with S1S_13.

Single-element realized gain for LPDAs of S1S_145–8.5 dBi is achieved over octave bandwidths, with beamwidths narrowing from S1S_1590° at the low end to S1S_1670° at the upper frequency for E-plane, and typically S1S_17 dB cross-polarization at boresight (Acedo et al., 2020, Seikh et al., 20 Jan 2026).

Polarization isolation is quantified by cross-polarization ratio (XPR) and purity metrics, e.g., S1S_18 and S1S_19 (Seikh et al., 20 Jan 2026). These parameters are validated through anechoic chamber measurements and full-wave simulation (e.g., HFSS, WIPL-D or NEC-4.2), yielding τ<1\tau<1095% agreement in amplitude and beam structure over 100–850 MHz (Seikh et al., 20 Jan 2026).

4. Calibration, Yield, and Validation Workflows

Absolute pattern calibration is critical for high-precision science applications. At AERA, an in-situ far-field calibration campaign employed an octocopter-drone to position a reference emitter above the array, measuring received power at known τ<1\tau<11 values to derive τ<1\tau<12 using a Friis-derivative relation (Briechle, 2016):

τ<1\tau<13

where τ<1\tau<14 is source-to-antenna range, τ<1\tau<15 received power, τ<1\tau<16 transmitter gain, τ<1\tau<17 transmit power. The achieved absolute amplitude uncertainty was 9.3%.

Workflow validation is performed by overlaying measured and simulated τ<1\tau<18 patterns (as in AERA, τ<1\tau<19 at n=1…Nn=1\ldots N0 is n=1…Nn=1\ldots N1 m, with n=1…Nn=1\ldots N2 residual to simulation across the scan) (Briechle, 2016). AAFIYA enables automated impedance, realized gain, and beam pattern validation, with yield estimation via Monte Carlo tolerancing of n=1…Nn=1\ldots N3 and n=1…Nn=1\ldots N4, supporting robust design under fabrication uncertainty. Standard metrics include pass/fail RLn=1…Nn=1\ldots N5 dB and specified minimum realized gain (Seikh et al., 20 Jan 2026).

5. Array Configuration and Mutual Coupling

Large-aperture LPDA arrays (e.g., SKA1-LOW) consist of quasi-random distributions (Halton or jittered-spiral) of n=1…Nn=1\ldots N6 LPDAs (e.g., n=1…Nn=1\ldots N7 per 35 m station). Mutual coupling is mitigated by >1.5 m minimum element spacing, randomized placement, and use of ground-screens beneath elements to reduce surface wave propagation (Acedo et al., 2020).

The total array pattern is given by n=1…Nn=1\ldots N8 with array factor n=1…Nn=1\ldots N9, where L1L_10 are complex weights, and L1L_11 the element response (Acedo et al., 2020). Spacing L1L_12 is chosen to balance grating lobe suppression (prefer L1L_13) and manageable coupling/costs (L1L_141.5–2 m is typical for 50–350 MHz) (Acedo et al., 2020).

6. Scientific Applications and Impact

LPDA stations are deployed in radio detection of cosmic-ray air showers, where absolute calibration of the vector effective length is required to reconstruct incident electric field amplitudes with systematics below L1L_15. At AERA, such calibration improved primary energy reconstruction uncertainty from L1L_1614% to L1L_1710%, with a L1L_1810–15 g/cmL1L_19 improvement in L1≈c/(2fmin)L_1\approx c/(2f_\text{min})0 resolution (Briechle, 2016).

SKALA4 LPDAs, as used in the SKA1-LOW array, provide wideband sky coverage matched to contemporary requirements in radio astronomy. Accurate impedance and beam control, together with validated cross-polarization and yield, are necessary for reliable signal extraction amid complex environments (Acedo et al., 2020). AAFIYA automation extends to future data-driven LPDA optimization and rapid prototyping workflows for coherent large-scale experiments (Seikh et al., 20 Jan 2026).

7. Practical Design Recommendations

Key design choices are summarized:

Parameter Typical Range Source
Scaling factor L1≈c/(2fmin)L_1\approx c/(2f_\text{min})1 0.85 (SKA4, AERA); 0.85–0.90 (general) (Acedo et al., 2020, Briechle, 2016, Seikh et al., 20 Jan 2026)
Apex angle L1≈c/(2fmin)L_1\approx c/(2f_\text{min})2 12°–15° (AAFIYA); 37° (SKALA4) (Seikh et al., 20 Jan 2026, Acedo et al., 2020)
# of elements L1≈c/(2fmin)L_1\approx c/(2f_\text{min})3 9 (AERA), 12 (SKA4), 16–20 (100–850 MHz) (Briechle, 2016, Acedo et al., 2020, Seikh et al., 20 Jan 2026)
VSWR L1≈c/(2fmin)L_1\approx c/(2f_\text{min})42:1 (full band) (Briechle, 2016, Acedo et al., 2020, Seikh et al., 20 Jan 2026)
Boresight gain 5–8.5 dBi (Acedo et al., 2020, Seikh et al., 20 Jan 2026)
Cross-pol ratio L1≈c/(2fmin)L_1\approx c/(2f_\text{min})5–20 dB (boresight) (Acedo et al., 2020, Seikh et al., 20 Jan 2026)

For validation, cross-calibration with full-wave simulation (HFSS, WIPL-D, NEC), Friis-based realized gain in anechoic conditions, and systematic tolerance-and-yield estimation are recommended for ensuring reproducible, publication-grade LPDA performance (Briechle, 2016, Seikh et al., 20 Jan 2026). All critical workflow steps can be encoded in reproducible scripts as demonstrated by AAFIYA’s minimal analysis template (Seikh et al., 20 Jan 2026).

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