Cylindrical Near-Field
How Cylindrical Scanning Reconstructs the Pattern
In a cylindrical near-field range the antenna under test rotates about a vertical axis while a stationary probe travels up and down a vertical rail. At each azimuth angle φ and each height z the receiver records both amplitude and phase of the two tangential field components. The result is a two-dimensional data matrix sampled on the surface of an imaginary cylinder of radius r0. Because the measurement plane is a regular grid in φ and z, the data can be processed with a one-dimensional discrete Fourier transform in azimuth and a continuous-spectrum integral in the axial wavenumber, making the computation efficient even for electrically large apertures.
The physics rests on cylindrical mode expansion. Any source-free field outside the smallest cylinder enclosing the antenna can be written as a sum of outward-traveling cylindrical waves indexed by an integer azimuthal order n and a continuous axial wavenumber γ. Hankel functions of the second kind, Hn(2)(κρ), describe the radial dependence. Measuring the field on one cylinder fixes the mode coefficients, and the far field follows directly because each cylindrical mode maps to a known angular contribution as the radial coordinate goes to infinity. The asymptotic form of the Hankel function supplies the stationary-phase result that turns the mode sum into the radiation pattern.
The number of significant azimuthal modes is governed by the cylinder radius. Modes with n much larger than k·r0 are evanescent and carry negligible energy, so the series truncates at N ≈ k·r0 plus a small safety margin. This truncation, combined with the λ/2 axial Nyquist limit, fixes the required sampling density and total measurement time.
Governing Mode Expansion and Sampling
E(ρ,φ,z) = ∑n ∫ an(γ) Hn(2)(κρ) ejnφ ejγz dγ, κ2 = k2 − γ2
Maximum azimuthal mode index:
N ≈ k × r0 + 10, with k = 2π / λ
Sampling criteria (no aliasing):
Δz ≤ λ/2 and Δφ ≤ 180° / N (so azimuth points ≥ 2N + 1)
Example: f = 10 GHz (λ ≈ 30 mm), r0 = 0.5 m → k×r0 ≈ 105, N ≈ 115, so ≈ 231 azimuth samples and Δz ≤ 15 mm. Far-field gain accuracy after probe correction is typically ±0.3 dB.
Near-Field Geometry Comparison
| Geometry | Scan surface | Pattern coverage | Positioner | Relative point count | Best-fit antenna |
|---|---|---|---|---|---|
| Cylindrical | Cylinder (φ, z) | Full azimuth, limited elevation | Rotation + vertical linear | Medium | Fan-beam, sectoral, broadcast |
| Planar | Flat plane (x, y) | Forward cone only (no back) | 2-axis linear scanner | Low to medium | High-gain pencil-beam apertures |
| Spherical | Sphere (θ, φ) | Complete 4π including back lobes | Two rotation stages | High | Low-gain, broad-beam, full 3D |
| Far-field range | Direct (R > 2D2/λ) | Direct pattern, no transform | Single rotation | Low | Small antennas, validation |
Frequently Asked Questions
When should I choose cylindrical near-field over planar or spherical scanning?
Cylindrical scanning suits fan-beam and sectoral antennas (base station panels, surveillance radar arrays, broadcast antennas) that are broad in azimuth and narrow in elevation. The cylinder captures the full 360° of azimuth while limiting the vertical scan to the energy-bearing elevation sector. Planar near-field fits forward-radiating pencil-beam apertures, while spherical near-field gives complete 4π coverage at the cost of far more points and a two-axis rotation positioner.
How fine must the cylindrical near-field sampling be to avoid aliasing?
The axial spacing must satisfy Δz ≤ λ/2, and the azimuth spacing follows the maximum mode index N ≈ k·r0 + 10, giving Δφ ≤ 180°/N and at least 2N+1 azimuth points. At 10 GHz with r0 = 0.5 m, k·r0 ≈ 105, so roughly 231 azimuth points and a 15 mm vertical step are needed. Undersampling either coordinate folds high-order modes into the visible region and corrupts the computed sidelobes.
Why does cylindrical near-field measurement require probe correction?
The probe has its own directive pattern and polarization response, so the measured signal is the convolution of the true field with the probe pattern in cylindrical modes. Probe correction divides the measured mode coefficients by the probe receiving coefficients to recover only the test antenna. An open-ended waveguide probe is favored for its smooth, easily deconvolved pattern. Skipping correction adds gain errors of several tenths of a dB and degrades sidelobe and cross-polarization accuracy.