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As a part of the research project in Denmark on spherical near-field measurements, a number of FORTRAN programs for transformation of measured near-field data has been developed since 1976. Based on earlier work by Jensen, Wacker and Lewis, the series of programs can be summarized as follows: SNIFT (1976) Without probe correction based on a program by Lewis, NBS. Small antennas only. SNIFTB (1977) First program with probe correction. Maximum antenna diameter 25 wavelengths due to numerical instabilities. SNIFTC (1978) With probe correction. Numerically stable. Antenna size limited by the requirement that a full sphere of measured data must be contained in core memory during execution. SNIFM (1980) Segmented program with segmentation of data written for a HP1000 computer only. Antenna diameter limited to 120 wavelengths due to certain arrays in addressable memory. The new computer program is based on the experience with spherical near-field measurements at the Technical University of Denmark.
Spherical near-field testing of antennas requires the acquisition of a great volume of data. In general, to compute the far-field of the antenna under test in any direction requires the acquisition of data at sample intervals related to the size of the antenna under test over a spherical sampling surface completely enclosing the antenna under test. This data must also be sampled as a function of probe orientation. Even for the simplest possible case, two probe orientations (or two probes) must be used.
A set of near-field measurements has been performed by combining the methods of non-probe-corrected spherical near-field scanning and gain standard substitution. In this paper we describe the technique used and report on the results obtained for a particular 24 inch 13 GHz paraboloidal dish. We demonstrate that the gain comparison measurement used with spherical near-field scanning give results in excellent agreement with gain comparison used with compact range measurement. Lastly we demonstrate a novel utilization of near-field scanning which permits a gain comparison measurement with a single spherical scan.
This paper reports on research being conducted at Georgia Tech on the spherical surface near-field measurement technique. The popularity of the spherical surface near-field measurement technique is indicated in the list of near-field ranges as shown in Table I. This popularity is, in large part, due to the availability of the scientific Atlanta Spherical Near-Field Antenna Analyzer. Specifically, the paper reports on the status of (1) the Georgia Tech spherical surface near-field range, (2) comparison of non-probe compensated spherical surface near-field to far-field transformation techniques, (3) a probe position error compensation technique for spherical surface measurements, and (4) alternative spherical surface near-field to far-field transformations which include probe compensation.
An 80 element linear phased array antenna was measured in the nearfield. The insertion phase and amplitude for each element were measured while the 8-bit ferrite phase shifters were individually stepped through their degrees for freedom.
Test techniques and test results will be presented on Compact Range testing of a 1.9m offset reflector at 20/30 GHz. The antenna is part of a demonstration model for an intersatellite link antenna system.
Acceptance testing of the AN/SYR-1 Electronically Steered Phased Array (ESPA) antenna in a Compact Antenna Range is described. Unique to the testing described are (1) generation of the beam steering commands to the phased array as well as control of the positioner and recording equipment by a single desktop computer and (2) the recording of S-band antenna patterns after down-conversion to a 300 MHz IF. Modifications and interfaces to the standard Compact Antenna Range equipment for testing of the multi-element planar phased array are described.
Conventional antenna test techniques – both far field “slant ranges” and near field – pose limitations for radiative RF testing of satellite antennas and payload systems, of increasing complexity in terms of size, operating frequencies, configurations and technology, particularly when such systems need to be evaluated in their “in-situ” locations on typical satellite platforms, in their flight configurations. Often, combination of tests and simulation has been the only recourse for evaluating system performance. In this paper, a methodology is proposed to achieve these test objectives via the use of a suitable configures, wideband, large (Quiet zone 7m x 5m x 5m), compact range for evaluation od system parameters like E.I.R.P., G/T, C/I, BER, and RF sensing performances. The test plan and evaluation schemes appropriate for these tests are elaborated to demonstrate the validity and usefulness of the approach. For some specific parameters like C/I (for a multibeam payload system) and the radar parameters (for a satellite borne radar system), it turns out that the proposed test methodologies offer the only realistic and complete tool for evaluating such system at satellite level.
A monostatic C.W. radar cross-section facility in the X-band at the Radar and Communication Centre, Indian Institute of Technology, Kharagpur, India is described. This set up is capable of automatically measuring the c.w. monostatic radar cross-section over the range of aspect angle 0 to ±180o for both TE and TM polarizations. The transmitting/receiving antenna and the rotating target is housed on the roof-top of the building and the microwave circuit with recording arrangement is in the air-conditioned laboratory. It is capable of handling a target of arbitrary shape of maximum size equal to 70 cm and uses a two-stage background (without target) cancellation technique employing Magic-T. A typical value of effective isolation between the transmitted and received signals is of the order of 70 dB and a dynamic range of 35 dB. Measurements made in this set up with different types of targets show a fair agreement with the results obtained by analytical investigations. The same set-up with necessary modifications for measuring the phase of the scattered field along with the amplitude data is expected to provide the amplitude and phase information for target identification and classification problems.
Spherical near-field testing and other specialized antenna measurements require precise range and positioner alignment. This paper presents a method based on optical techniques to conveniently measure and monitor both range alignment and the positioner axis orthogonality and intersection. The hardware requirements consist of a theodolite and a unique target mirror assembly viewable from either side.
The loop cell is fabricated using two intersecting metal sheets joined at the intersection and forming a 36 deg angle. A section of a loop is mounted between two coaxial panel jacks, one on each sheet at a distance equal to the loop radius from the intersection. A known current through this section of electrically small loop produced calculable E and H fields between the sheets in the plane of the loop. These known fields may be used to determine the antenna factor of small E and H antennas placed in the field if the mutual impedance due to the antenna images in the sheets is negligible and the antenna is not close to the open edges of the cell. Measured and calculated antenna factors agree within ±2 dB between 0.25 MHz and 1000 MHz.
The development of a high resolution instrumentation radar is described. This radar constructed at X-band uses a chirp waveform to achieve a 4.9” range resolution capability. A key feature of this development is the use of cos2 x amplitude weighting to control the range sidelobes. An example of a high resolution radar response is described.
Far field antenna radiation patterns of vehicle mounted antennas are often recorded on the antenna range by rotating the entire vehicle/antenna system with a multiple axis vehicle positioner. Antenna patterns, obtained in this manner, consider the antenna and vehicle as a system and include the effects of the vehicle structure. These patterns are more representative of the operational antenna patterns than the “free space” patterns of the antenna itself. When the antenna is arbitrarily directed on the vehicle, standard antenna pattern cut trajectories, recorded in the coordinate system of the vehicle, become skewed when referenced to the coordinate system of the antenna. With proper adjustment of the fixed angles of the vehicle positioner however, selected standard antenna pattern cut trajectories, referenced to the antenna, may be obtained. The required fixed vehicle positioner angles are obtained from solutions to systems of equations representing the coordinate transformations for the positioner/vehicle/antenna system. In this paper, two general methods of obtaining the coordinate transformation equations are reviewed. These equations are then solved to obtain expressions for the positioner angles necessary for specific cut trajectories. A practical example of a six axis transformation associated with measurements of a three axis gimballed aircraft mounted radar antenna and a three axis vehicle positioner is used to illustrate the techniques (This example was taken from a recent RADC/Newport measurement program.
A strong emphasis is now being placed on techniques for reduction of radar cross-section. A missile or aircraft which is invisible to radar has an important strategic advantage. With this fact in mind, the user of a weapons system may place an upper limit on the radar cross-section that he will permit his missile or aircraft to have. The designer must then make use of “stealth technology” to reduce the cross-section to an acceptable level. In order to verify the design, radar cross-section measurements must be made. Thus the current emphasis on cross-section reduction leads to an important need for accurate and reliable methods of measuring radar cross-section.
Scientific-Atlanta, Inc. was selected by the United States Air Force to design and install a complete turn-key test facility for depot maintenance support of the F-16 fighter aircraft. These facilities have been installed at Hill Air Force Base, Utah. Four complete facilities have been supplied, each consisting of a Series 2020 Antenna Analyzer and a Series 5750 Compact Antenna Range. Two facilities are configured for antenna testing and two for radome testing. This paper describes the equipment furnished for this program. The hardware is discussed as well as the special software designed to perform specific radome and antenna tests.
An instrument has been built which allows the electromagnetic measurement of the surface accuracy of a large millimeter-wavelength antenna. The University of Texas 4.9 m radio telescope has been measured with this technique at 86.1 GHz to an accuracy of 4 µm at the surface. Our technique is an interferometric one which is fast, accurate, and able to measure the whole antenna surface at once. While the technique is illustrated by its use on a large antenna, it could be used in a near field measurement of a smaller antenna. Several antenna surface maps are presented. A comparison of run-to-run repeatability was made. The technique itself was tested by deforming the antenna surface in a known way and subsequently detecting the deformation. In addition, important factors which influence the overall error budget have been identified. These include errors in setting the antenna angular position and fluctuation noise in the atmosphere and electronics. An instrument has been built which allows the electromagnetic measurement of the surface accuracy of a large millimeter-wavelength antenna. The University of Texas 4.9 m radio telescope has been measured with this technique at 86.1 GHz to an accuracy of 4 µm at the surface. Our technique is an interferometric one which is fast, accurate, and able to measure the whole antenna surface at once. While the technique is illustrated by its use on a large antenna, it could be used in a near field measurement of a smaller antenna. Several antenna surface maps are presented. A comparison of run-to-run repeatability was made. The technique itself was tested by deforming the antenna surface in a known way and subsequently detecting the deformation. In addition, important factors which influence the overall error budget have been identified. These include errors in setting the antenna angular position and fluctuation noise in the atmosphere and electronics.
This paper explored the details of the mechanical and electrical design of a multipurpose scanner. Planar, cylindrical and spherical scans as well as separation scanning (for extrapolation gain method) are accomplished by allowing any two of the five axes to be selected for program control. Special laser interferometers are available for the X-Y planar scanning. However, all axes are fitted with two-speed synchros. The method of driving and counter-weighing the X-Y probe carriage reduced the moving mass significantly which helps in the areas of start-stop agility, resonances, bearing wear and structual bending.
The Naval Underwater Systems Center has under construction an antenna pattern arch for measuring the radiation pattern of submarine antennas protruding above the sea water surface. The 70-foot radius tripodal arch is constructed of laminated wood members located over a 66-foot by 93-foot concrete pool which will contain a six inch depth of sea water. A well is located off-center in the pool for mounting the antenna under test. Pattern measurements will be made from 20 MHz to 2 GHz and at antenna heights of up to 15-feet above the sea water. Heretofore this over-sea water pattern information has been unobtainable. The important criteria for far-field antenna measurements are mentioned. The Numerical Electromagnetic Code (NEC) was used to model typical submarine antennas at various frequencies in order to predict the accuracy of the arch range. NEC uses moment methods to determine the arch patterns and the far-field patterns.
The operation and application of the Scientific-Atlanta Model 1784/ 1785 Millimeter-Wave to Microwave Converter is discussed. The converter allows single channel or multi-channel coherent measurements to be made with excellent sensitivity at Millimeter-wave frequencies. The converter improves the dynamic range of Millimeter-wave measurements by up to 30 dB over conventional measurements made with broad-band microwave receivers operating at high mixer harmonic numbers.
Test results will be presented for a four foot S-Band reflector antenna together with the compact range modification and test verification at 2.2 GHz. Similarly compact range test results will be presented for an eight foot K-band reflector antenna at 23 GHz.