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As the need for taking antenna measurements moves indoors, the antenna engineer must begin to work with a variety of constraints. Many of these constraints are directly related to facilities considerations. Often the current chamber size is not possible due to the available spaces within one’s organization. Perhaps a new building or an addition onto an existing building is possible, but more often than not the antenna engineer is faced with a number of sites that are “close” to his/her ideal model. But how does one valuate the tradeoffs? What are the ramifications of changing the performance characteristics, the size of the Quiet Zone, or the frequency of operation? What would happen to the size and price of a facility if the performance changed from an 8 foot Q.Z. down to a 2 GHz to a 6 foot Q.Z. down to 1 GHz? Is there a model to help sort out some of these issues. This paper will present a model to help the engineer sort out these issues in an organized manner.
A major objective in the design of an RCS measurement facility is to obtain the greatest possible productivity (overall measurement efficiency) while maintaining the accuracy and sensitivity necessary for low radar cross section targets. This paper will present parameters affecting the total throughput rates of an indoor facility including instrumentation, target handling, and band changes-one of the most time consuming activities in the measurement process. Sensitivity and accuracy issues to be discussed include radar capabilities, feeds and feed clustering, compact range, background levels, and diffraction control.
Mechanical and environmental considerations for outdoor operation of an inflatable column are discussed in the context of a 30-ft-high column. The column is designed to support a 900-lb load in a 30-knot wind. Column RCS is less than -40 dBsm below 1 GHz for both horizontally and vertically polarized illumination. Designs using Mylar and Teflon-coated Kevlar as skin materials are compared. The primary concerns are wind loading, pressure regulation, and solar heating. Wind effects include static loading, gusting, and vortex shedding. In addition, wind-driven particulates, such as sand or stones propelled by passing vehicles can puncture the column. A pneumatic control system maintains a constant internal support pressure in the presence of leaks or pressure fluctuations due to changes in solar illumination.
This system provides improved techniques for controlling positioning axes, and secure transmission of position data from remotely located control systems. Advancements in controls technology have allows more complex configurations for use in the manipulation of RCS targets in indoor ranges. This paper will discuss a unique system design that provides automated testing and positioning of RCS test bodies. The current system uses seven axes of motion, and allows for simultaneous motion as well as synchronous motion of any axis pairs in the system. These axes include Target azimuth and elevation, Pylon azimuth and elevation, Upper and Lower turntable azimuth, and carriage linear drives. In addition, the concepts of secure data transmission through the use of specialized fiber optics are addressed. Finally, a complex set of safety interlocks and man and machine protection is discussed. The entire system is currently implemented and running in the Boeing range.
The Hughes Aircraft Company recently completed the design, development, and construction of a new engineering facility that is dedicated to providing state-of-the-art Radar Cross Section Measurements. The facility is located at the Radar Systems Group in El Segundo, California and consists of two secure, tempest shielded anechoic chambers, a secure high bay work area, two large secure storage vaults, a secure tempest computer facility, a secure conference room, and the normal building support facilities. This RCS measurement test facility is the result of Hughes committing the time and money to study the problems which influence user friendly RCS measurement facility design decisions. Both anechoic chambers contain compact ranges and RCS measurement data collection systems. A description of the facility layout, instrumentation, target handling capability, and target access is presented.
There are two main parts to an antenna or RCS measurement system: the measurement instrumentation, and the measurement environment or “range”. Performance of the measurement system is dependent upon both the instrumentation and the range. Developing a successful measurement system requires understanding both parts of the system. This paper describes a Compact Test Range that has been designed and built for the purpose of demonstrating antenna and RCS measurement performance of a complete measurement system. Additionally the Compact Test Range will serve as a development platform for future antenna and RCS products and systems. The purpose of the chamber, design objectives, design techniques, expected and measured performance are all discussed.
Lockheed’s Advanced Development Company (LADC), located in Burbank, California, has recently completed construction of a state-of-the-art indoor Antenna/RCS test facility. This facility is housed in a dedicated 40,000 square foot building which is a maximum of 80 feet high. This building contains three anechoic chambers providing Antenna/RCS measurement capability from 100 Mhz to 100 Ghz. The largest chamber, with dimensions of 64 feet by 64 feet by 97 feet is configured as a compact range. This chamber utilizes the largest collimating reflector that Scientific-Atlanta has ever constructed. Primary test usage of this chamber is for RCS measurements in the frequency band of 700 Mhz to 100 Ghz. The second chamber is configured as a tapered horn test range. Its dimensions are 155 feet long with a 50 foot by 50 foot by 55 foot volume measurement zone. This chamber is utilized for RCS tests in the VHF, UHF, and L frequency bands and antenna tests from 100 MHz and up. The third chamber, with dimensions 14 foot by 14 foot by 56 foot, is a far field chamber designed to check out and evaluate small items up to 100 GHz. The entire facility has been designed to maximize efficiency, minimize the cost of operation, and produce outstanding quality data from Antenna/RCS measurements. A number of innovative techniques in model handling, model access, and model security were incorporated into the facility design. These features, as well as utilization of unique Lockheed designed and built pylons, allowed achievement of all these goals.
The Dassault Electronique flexible near-field antenna test facility, ARAMIS, has been used for test and calibration of state-of-the-art active phased-array antennas which were designed for military SATCOM operation. The 14-month successful program dramatically emphasized the benefits of a flexible antenna test facility such as ARAMIS. These benefits are the following: • Flexibility o Far-field mode (test of radiating elements and modules) o Planar near-field mode (test of sub-arrays and complete antenna) o High-resolution field mapping mode o Array Element testing • Speed: quick mode switching, “on the fly” multiplexed acquisition • Versatility: calibration of a module, a sub-array and the antenna; radiation patterns; gain; faulty element detection • Productivity: a single indoor facility performing different types of measurements, integrated software Test results gathered during this program and showing the ARAMIS contribution are presented.
Among its different facilities, C.E.A. has an indoor range for radar cross section (RCS) measurements over a wide frequency range from 0,1 GHz to 18 GHz. The dimensions of this anechoic chamber, 45m x 13m x 12m and a quiet zone diameter of about 3m, make it one of the largest in Europe. It consists in a parabolic reflector for frequencies higher than 0,8 GHz and a system using inverse synthetic aperture radar (ISAR) techniques for lower frequencies associated with a short pulse coherent radar instrumentation equipment. In addition to performant instrumentation and illumination systems, the main features of this installation dedicated to measure stealth objects, are low residual clutter, discrete target supports, and powerful processing software. The technical solutions adopted are described.
An HP 8510B based RCS measurement system is presented. It can be operated in CW, hardware gating, and fast-CW modes. A VAX-3800 computer and a MAP 4000 array processor are used to speed up the data analysis and a PS 390 graphic system is used to display graphic. Three ISAR techniques, i.e., DFT approximation, focusing image processing, and diffraction limited methods, are available in the analysis program to get the target image. With an amplitude taper removing technique, this system can measure large target whose size is almost up to the size of compact range reflector.
British Telecom Research Laboratories (BTRL) operate two outdoor test ranges. One of the rages is a fully automated, well characterized, 670m Ground reflection range operating from 0.1 to 26.5 GHz, which can take antennas up to 5.5m diameter (4500 kg). This range can produce u to 100 dB of dynamic range using the time-domain gating facilities available with an HP8510B vector network analyzer, and a crosspolar purity of better than -50dB is achievable. The second test range is 100m in length and can handle antennas of up to 1.8m diameter (500 kg). It operates over the frequency range 0.8 to 40 GHz.
Accurate near-field cross-polarization measurements on circularly polarized (CP) antennas at millimeter-wave frequencies require well-characterized probes with low axial ratios. We have recently obtained and calibrated dual-port CP horns for use as near-field probes at frequencies of 40-50 GHz. These horns have axial ratios which are 0.3 dB or less over a 10% frequency bandwidth. With these good axial ratios the difference between vector and scalar probe correction is usually small. Additional advantages of the dual-port probes are the need for only a single alignment, more accurate knowledge of the relative phase between two ports of the same probe, and the ability to obtain both main and cross polarized data during one scan. The axial ratios of the dual port CP probes are also better than those of single-port CP Probes. In this paper we present some gain, axial ratio, and pattern measurements for these probes and show that they give accurate cross-polarization measurements.
Airborne or spaceborne radar systems often require adaptive suppression of interference and clutter. Before the deployment of this adaptive radar, tests must verify how well the system detects targets and suppresses clutter and jammer signals. This paper discusses a recently developed focused near-field testing technique that is suitable for implementation in an anechoic chamber. With this technique, phased-array near-field focusing provides far-field equivalent performance at a range distance of one aperture diameter from the adaptive antenna under test. The performance of a sidelobe-canceller adaptive phased array antenna operating in the presence of near-field clutter and jamming is theoretically investigated. Numerical simulations indicate that near-field and far-field testing can be equivalent.
The near field technique has grown from experimental systems of the early 1960s to sophisticated accepted means of testing antennas. Several schemes have been employed, namely planar, cylindrical and spherical scanning. The spherical scanning system chosen for one of the near field ranges at GE Aerospace is different from most near field systems in that the test antenna remains stationary while the probe is made to scan over a surface of an imaginary sphere surrounding it. The sampled field is corrected for positional, phase and amplitude errors and transformed to the far field. Radiation patterns, gain, EIRP, group delay and amplitude response were measured for a shaped beam communications antenna.
Near-Field antenna measurements were made using a Hewlett Packard 8510 automated network analyzer. This system features measurement sensitivity better than -90 dBm at measurement speeds of one data point per millisecond in the fast data acquisition mode. The system was configured using external, even harmonic mixers and a fiber optic distributed local oscillator signal. Additionally, the time domain capability of the HP 8510, made it possible to generate far-field diagnostic results immediately after data acquisition without the use of an external computer.
Effects of probe position errors in planar near-field measurements have been significantly reduced at NIST by accurate alignment of the scanner and an analytic error correction. Currently, the near-field range has probe position errors greater than 0.01cm only at the edges of the 4 x 4 m2 area, and less than that everywhere else. The position errors can be further removed by a theoretical procedure, which requires only the error-contaminated near-field and the probe position errors at the points of measurements. All necessary computations can be efficiently performed using FFTs. An explicit nth-order approximation to the ideal near field of the antenna can be shown to converge to the error-free near fied. Computer simulations with eriodic error functions show that this error-correction technique is highly successful even if the errors are as large as 0.2wavelength, thereby making near-field measurements at frequencies will abobe 60 GHz more practicable.
Antenna engineers recognize that the planar near-field method for calibrating antennas provide accurate pattern and gain measurements. Bothe the pattern and gain measurements require some degree of probe position accuracy in order to achieve accurate results. This degree of accuracy increases for antennas that have structured near-field patterns. These are antennas in which the amplitude and phase change rapidly over a very small position change in the near-field scan plane. The National Institute of Standards and Technology (NIST) has recently measured an antenna with a very structured near-field pattern. This measurement was performed using a new probe positioning system developed at NIST. This measurement will be discussed and results will be presented showing how slight probe position errors alter the antenna pattern and gain.
We have developed planar near-field codes, written in Fortran 77, to serve as a research tool in antenna metrology. This new package has a highly modular structure and can be used to address a wide variety of problems in antenna metrology. We describe some of the inner workings of the codes, the data management schemes, and the structure of the input/output sections to enable scientists and programmers to use these codes effectively. The structure of the code is open, so that a new application can be incorporated into the package for future use with relative ease. A new module can rely on the large number of reusable subroutines currently in existence, and new routines are easily integrated into the existing library. Examples of applications of the codes to basic research problems, such as transformation of a near field to the far field and probe position error correction, are used to illustrate the effectiveness of these codes. Sample outputs are shown. The advantage of a high degree of modularization is demonstrated by the use of DOS batch files to execute Fortran modules in a desired sequence.
A new spherical near field facility has been recently implemented at the Electromagnetic Propagation Area of INTA. The facility makes use of an existing big anechoic chamber (12 x 12 x 12 m.) and the near field/fair field transformation software developed by TICRA. This range has been calibrated by measuring an offset reflector antenna and comparing the results with those obtained in previous measurements of this antenna in other European testing facilities of different types. An experimental study has been carried out to check the dependence of the transformation software on the scanning parameters and different misalignments have been produced in order to determine the impact of the mechanical deformations on the accuracy of the system.
A near field synthetic aperture imaging technique using three main beam suppression methods is used to locate and quantify the sources of stray signals in a compact range. First, main beam cancellation by subtracting the complex average of the measured field for the overall probe aperture is used. Second, a software on-axis null is generated by preprocessing the data. Third, an antenna with a broadside null is used as the prober. It is shown that the software on-axis null enhances the resolution of the spurious scatterer images and is able to detect small spurious scattering centers, such as the surface discontinuity at the top of the reflector, which are otherwise undetectable. Probe data with two metallic tapes placed on the compact range reflector is used as another example to show the performance of the nulling technique.