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M. O'Brien (Loran Randtron Systems),R. Magatagen (Loran Randtron Systems), November 1989
This paper describes the techniques applied to a fully automatic computer controlled, HP8510 based, range gated digital data acquisition system used to provide scale modeled large aperture synthesis, evaluation of aircraft blockage effects, array patterns, element cancellation ratios, as well as providing a large accurate data base for radar simulation exercises.
H.D. Griffiths (University College London),A.L. Cullen (University College London),
E.H. England (Admiralty Research Establishment),
E.T. Calazans (University College London),
R. Benjamin (University College London), November 1989
A technique is presented for the measurement of antenna patterns, in which a long, thin wire is moved past the antenna aperture while the changes in reflection coefficient at the antenna feed are recorded. By suitable processing of these data, the antenna pattern can be calculated.
S.W. Gilmore (The Ohio State University ElectroScience Laboratory),R.C. Rudduck (The Ohio State University ElectroScience Laboratory), November 1989
A microwave holographic analysis system is shown to have successfully resolved the surface deformations on an 8' symmetric Cassegrain reflector antenna known to have significant surface deformation problems. The technique is based on the Fourier transform relationship between the aperture field of an antenna and its radiated far-zone field. A signal processing technique dubbed "pattern simulation and subtraction" is discussed that increases the resolution in the transformed aperture domain by removing unwanted signals from the aperture distribution. Measurements taken on the Cassegrain reflector at 11 GHz in the OSU-ESL Compact Range provided excellent amplitude and phase stable data to be processed by the holographic analysis system. Surface deformation profiles generated by this system were then compared to an optical measurement of the main reflector surface. Excellent agreement was obtained with a worst case deviation in the adjusted profiles being 0.05 ?.
R.C. Rudduck (The Ohio State University ElectroScience Laboratory),K.M. Lambert (ANALEX Corporation),
T-H. Lee (The Ohio State University ElectroScience Laboratory), November 1989
An overview of results are presented for far field pattern, antenna gain and antenna temperature measurements of reflector antennas in several frequency bands. The pattern and gain measurements were taken in the compact range at The Ohio State University. The dynamic range available, which gives the ability to take a full 360 degree pattern, and the relatively high speed at which data is collected, are major advantages for pattern and gain measurements in the compact range. In a series of related measurements an 8-foot diameter Cassegrain reflector was used for antenna temperature measurements under clear weather conditions in an outdoor environment.
J. Saget (Electronique Serge Dassault), November 1989
In the last few years, the interest in millimeter wave systems, like radars, seekers and radiometers has increased rapidly. Though the size of narrow-beamwidth antennas in the 60-200 GHz range is limited to some 20 inches, an accurate far-field antenna test range would need to be very long.
The achievement of precision antenna pattern measurements with a 70' or even longer transmission length requires the use of some power that is hardly available and expensive.
A cost-effective and more accurate solution is to use a lab-sized compact range that presents several advantages over the classical so-called far-field anechoic chamber: - Small anechoic enclosure (2.5 x 1.2 x 1.2 meters) meaning low cost structure and very low investissement in absorbing material. No special air-conditioning is needed. This enclosure can be installed in the antenna laboratory or office. Due to the small size of the test range and antennas under test, installation, handling and operation are very easy.
For spaceborne applications, where clean environment is requested, a small chamber is easier to keep free of dust than a large one.
- The compact range is of the single, front fed, paraboloid reflector type, with serrated edges.
The size and shape of the reflector and serrations have been determined by scaling a large compact range of ESD design, with several units of different size in operation.
The focal length of 0.8 meter only accounts in the transmission path losses and the standard very low power millimeterwave signal generators are usable to perform precision measurements.
The largest dimension of the reflector is 1 meter and this small size allows the use of an accurate machining process, leading to a very high surface accuracy at a reasonable cost. The aluminum alloy foundry used for the reflector is highly temperature stable.
- Feeds are standard products, available from several millimeter wave components manufacturers. They are corrugated horns, with low sidelobes, constant and broad beamwidth over the full waveguide band and symmetrical patterns in E and H planes.
- The compact range reflector, feeds and test positioner are installed on a single granite slab for mechanical and thermal stability, to avoid defocusing of the compact range.
- A micro-positioner or a precision X Y phase probe can be installed at the center of the quiet zone. Due to their small size, these devices can be very accurate and stable.
Due to the compactness of this test range, all the test instrumentation can be installed under the rigid floor of the enclosure and the length of the lossy RF (waveguide) connections never exceeds 1 meter.
This paper discusses the results of a recent study on the UHF performance of a Harris Shaped Compact Range. The design process for the dual polarized, 70% bandwidth UHF feedhorn is summarized. Measured data is presented for primary feedhorn patterns and for one-way CW field probe measurements with open-ended waveguide. The measured data is overlaid with computer predictions to validate the modelling tools and the measurement procedures. The automated quiet zone characterization procedure for amplitude and phase is also discussed.
H.M. Aumann (Massachusetts Institute of Technology),F.G. Willwerth (Massachusetts Institute of Technology), November 1989
Performance verification of an adaptive array requires direct, real-time sampling of the antenna pattern. For a space-qualified array, measurements on a far-field range are impractical. A compact range offers a protected environment, but lacks a sufficiently wide field of view. Conventional near-field measurements can provide antenna patterns only indirectly.
This paper shows how far-field antenna patterns can be obtained in a relatively small anechoic chamber by focusing a phased array in the near-field. The focusing technique is based on matching the nulls of far-field and near-field antenna patterns, and is applicable to conformal or nonuniform phased arrays containing active radiating elements with independent amplitude and phase control.
The focusing technique was experimentally verified using a 32-element, linear, L-band array. Conventionally measured far-field and near-field patterns were compared with focused near-field patterns. Very good agreement in sidelobe levels and beamwidths was achieved.
L.D. Poles (Rome Air Development Center), November 1989
A special purpose 80 element linear phased array antenna was aligned using an iterative phase cycling method. First, the array was aligned to yield maximum main-beam power in the reactive near-field zone and then in the far-field zone. A record of the phase-shifters settings achieved for each zone was kept for use as look-up table during operation. In situ electronic main-beam steering was performed to compare sidelobe performance for the two cases. This report describes the measured results obtained using the phased cycling alignment procedure and compares the measured one-way radiation pattern for the two distance conditions.
G.E. Evans (Westinghouse Electric Corporation),A. Sullivan (Westinghouse Electric Corporation),
A.J. Johnson (Westinghouse Electric Corporation), November 1989
Scatter from the nearby obstacles on a pattern test range has been removed by synthesizing a short pulse with 16 CW measurements. With suitable weighting, a low time-sidelobe pulse, is synthesized to remove scatter to close as 25' for a 32' low sidelobe UHF array. In addition to the pulse results, equivalent CW data is extracted with an FFT from frequency to time, truncation, and in inverse FFT back to individual frequencies. The time samples provide considerable insight into the source of reflections at the range.
The procedure gives good agreement with CW patterns taken in another manner. It does so with a minimum of range modification, and operates at very low sidelobe levels.
J.M. Schuchardt (American Electronic Laboratories),D.J. Martin (American Electronic Laboratories), November 1989
In this paper the initial construction and validation phase for a new elevated outdoor antenna range is described. The facility is designed to provide excellent pattern, gain and reflection measurements in the 20 MHz to 40 GHz frequency range for apertures and arrays up to D = 16 feet in length.
Shown in detail is a physical description of the facility and equipment, an error budget and the results of field probing and antenna measurements. A discussion of the results shows a facility capable of antenna measurements at S/N levels of 60 dB providing a dynamic range of over 40 dB with error levels less than plus-or-minus 0.44 dB. Throughout the discussion, special attention is given to the full automation of the range in Phase 2 and its possible use for radar cross section measurements.
L.H. Hemming (McDonnell Douglas Technologies Incorporated), November 1989
In an industrial park, a clear area sufficient for antenna measurements is very hard to find and even more difficult to justify. The solution to this problem was to use the roof of a large industrial building. To avoid the reflections from industrial stacks used for air conditioning and spray booths and to provide a flat surface sufficient for good ground reflection operation, an elevated ground reflection antenna range was constructed. The range consists of a ground screen 40 feet by 110 feet mounted on a metal framework 14 feet high. A telescopic source antenna tower is located at one end of the range, and an azimuth-over-elevation antenna positioner with a model tower is located on a raised platform at the other end of the range. The range was evaluated using a lightweight field probe and the experimental data compared to calculated data derived from the NEC-BSC2 computer code. An analysis was made of the probe data defining the sources of extraneous energy and their possible reduction. Pattern comparison data is given to illustrate the correlation between the field probe data and the actual uncertainty experienced in making UHF antenna pattern measurements on the elevated ground reflection range. Finally, planned physical improvements to the range are discussed.
T.A. Millington (Southwest Research Institute), November 1989
At Southwest Research Institute, an automated antenna performance evaluation system has been developed for evaluation of mast-mounted direction finder antennas. This system utilizes a dual-channel receiving system and IF processor with off-line antenna pattern analysis software. Antennas are mounted on a test range which includes computer-controlled antenna positioners, test frequency transmitters, and a data acquisition equipment group. Amplitude and phase data is digitized and recorded for automated off-line antenna performance evaluation. The evaluation software provides a Fourier analysis of the antenna patterns which characterize distortion, alignment, relative phase relationships, amplitude mismatch, and bearing deviations (from theoretical values) for each antenna array.
The Vulnerability Assessment Laboratory (VAL) anechoic chamber at White Sands Missile Range, New Mexico was reconfigured and refurbished during the last part of 1988. This paper will be a facility description of the state-of-the-art Special Electromagnetic Interference (SEMI) investigation facility. Electromagnetic susceptibility and vulnerability investigations of US and, in some cases, foreign weapon systems are conducted by the EW experts in the Technology and Advanced Concepts (TAC) Division of VAL. EMI investigations have recently been completed on both the UH-50A BLACKHAWK and AH-64A Apache helicopters in the chamber.
The paper will cover the facility's three anechoic chambers, shielded RF instrumentation bay, computer facilities for EM coupling analyses, and the myriad of antenna, antenna pattern measurement, amplifier, electronic, and support instrumentation equipment for the chambers. A radar cross section measurement and an off-line RCS data processing station are also included in the facility.
Large arrays require large separations between the transmit antenna and the antenna under test (AUT) to measure pattern parameters in the far field. For the subject AUT, a range of 6 miles with a spurious signal level of -58 dB was necessary to obtain the required accuracy.
Measurements have been performed on a significantly shorter range without serious degradation. The antenna was focused for the angle of electronic scan and the resulting pattern measured. The theoretical far field patterns were compared with the calculated focused patterns for the short range. The maximum sidelobe error of 1/2 dB occurred at 60 degrees scan. There was no noticeable degradation in beamwidth, gain, or foresight at any scan angle. A 6-mile range would have produced a 2-dB sidelobe error.
The measured range reflection level was -50 dB. The transmit dish with sidelobes of 22 dB was replaced with an array that had 40 dB sidelobes. This change reduced the reflections to below the required -58 dB.
The antenna was focused using a range calibration technique and the measurements substantiated the theory.
The purpose of this paper is to discuss the accuracy requirement of a generic measurement system for in-flight antenna pattern evaluations. Elements of the measurement technique will be described. An attempt is made to distinguish the measurement requirement for a narrow beam radar antenna in contrast to that for broad beam communication antennas. Major elements of the measurement technique discussed include the flight path geometry, the multipath propagation problem, and the measurement errors. Instrumentation requirements consist of the ground segment, the receive and the tracking subsystems, and the airborne equipment, the radar components and the navigation and attitude sensors. Considering the in-flight antenna pattern testing as a generalized antenna range measurement problem, various sources of measurement errors are identified. An error budget assumption is made on each error component to estimate the overall expected accuracy of the in-flight antenna pattern measurement.
P.A. Langsford (GEC-Marconi Research Centre),M.J.C. Hayes (GEC-Marconi Research Centre),
R. Henderson (GEC-Marconi Research Centre), November 1989
A 400 element phased array antenna has been constructed at the GEC-Marconi Research Centre. Each radiating element is fed from its own phase shifter. The radiation patterns of this array have been measured using a recently constructed Cylindrical Near Field Test Facility.
The radiation pattern is obtained on a two dimensional grid and contains both amplitude and phase information. It is therefore possible to transform these data back to the array aperture to obtain the array excitation amplitudes and phases. The spatial resolution obtained in the aperture is a function of the angular coverage of the radiation pattern used.
The effect of deliberately introduced phase errors on the calculated aperture data is shown.
E.H. England (Admiralty Research Establishment),R. Young (Plessey Radar Limited), November 1989
Separation of the Antenna from the remainder of the system is not possible with a fully active phased array such as MESAR, since each array element has an associated electronic module which contains amplifiers (separate for transmit and receive), phase shifters, switches, etc. The "antenna" is therefore not reciprocal and it also requires a control system. As a result, the system used for pattern acquisition is considerably more complex than that used for testing conventional antennas and some of the traditional parameters are either not obtainable or require redefining. The methods used for testing the MESAR antenna are given together with details of the range equipment involved.
R.E. Shields (CSIRO Division of Radiophysics, Australia),G.M. Simms (CSIRO Division of Radiophysics, Australia), November 1989
The hardware and software developments undertaken to upgrade two far-field measurement facilities - a 12-m anechoic chamber and a 35-m outside range - are described. A method (termed quasi-far-field, QFF) for deriving antenna far-field patterns from a single plane scan at a distance less than the traditional distance of 2D2/? is described. The QFF technique involves pattern sample and subsequent pattern transform and reconstruction, from the easement distance to the far-field distance. A discussion of the limitations inherent in the QFF transform, including range length, is given. Experimental results for measurements made on circular-aperture antennas with both symmetric and asymmetric illumination, and on antennas with elliptical apertures, are described.
K. Wu (Electrospace Systems, Inc.),S. Parekh (Electrospace Systems, Inc.), November 1989
For transforming a Fresnel region pattern to a far-field pattern, we present here two methods, the "discrete beam sampling" method (DBSM) and the "displaced beam" method (DBM), which allow an accurate characterization for both linear as well as circular antenna apertures. Both methods assume a simple Fourier transform relationship between the aperture field distribution and the far-field of the antenna. The Fresnel region field is then essentially perturbed by an aperture quadratic phase error assumed to exist because of the finite distance at which the field pattern is characterized. Numerical simulation and its results are presented to show the accuracy of the reconstructed far-field data. Finally, an error analysis is performed to show the sensitivity of the above two methods.
Y. Rahmat-Samii (University of California Los Angeles), November 1989
The nonuniform sampling technique utilizes measured (or simulated) amplitude and phase far-field data at nonuniformly sampled data points and constructs the pattern from these limited number of measured data. The technique relies on the fact that the antenna far-field pattern is proportional to the Fourier transform of a function which is related to the induced current on the antenna. The application of nonuniform sampling technique becomes important in the situation for which it will be difficult (or impossible) to measure the far field at regular intervals.
In this paper, the application of the nonuniform sampling technique is demonstrated for antenna pattern measurements. The foundation of the technique is first reviewed and the required mathematical steps for the implementation of the technique is summarized. Both one dimensional and two dimensional cases are reviewed with attention given to the applicability of closed form expressions for the determination of the sampling coefficients. Numerical results are presented and comparison to measurements are shown. In particular, the application of this technique to a recently proposed space-station based antenna experiment is presented.
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