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The interdependence of accuracy and speed should be considered when analyzing measurement requirements. Tradeoffs can be made to optimize the measurement when accuracy is of primary importance, or where speed is critical. Several different measurement modes of the HP 8530A Microwave Receiver are presented, each with different measurement speed and accuracy tradeoffs. Examples are given that illustrate which acquisition modes would be appropriate to optimize the acquisition speed and accuracy in a variety of applications
This presentation offers some examples of performance in accomplishing high volume testing under the rigorous technical constraints imposed by the satellite industry. As an example of a high speed system, the Scientific-Atlanta Model 2095 will be used to illustrate the capability offered by today's technology. This system has found applicatio0n in the facilities of five satellite manufacturers constructed within the past three years and is proven by its demonstrated application in satellite programs.
This paper demonstrates modem parametric modeling techniques that can be used to form high resolution ISAR images of full scale flying aircraft. Both parametric spectral estimation techniques and autoregressive data extrapolation techniques are shown. We demonstrate imaging. In each case, the modem spectral estimation or data extrapolation techniques produce higher image resolution than that which is obtained by classical Fourier techniques.
A Superresolution technique for estimation of the time-delays, and amplitude/phase dispersion of the electromagnetic scattering is presented. In order to estimate the frequency dependence of individual scattering features, a pre-processing technique for the MUSIC (Multiple SIgnal Classification) algorithm is developed and applied to the theoretical and experimental scattering data.
Effectiveness of data extrapolation to generate high resolution radar images is studied. It is shown that polar formatted scattered field data can be extrapolated more effectively than (f, 0) domain scattered field data. The reason for this is that the forward backward linear prediction is not suitable for extrapolating the scattered field data with respect to aspect angle (0). Also, when the scattered field data is extrapolated with respect to frequency to increase the down range resolution, there can be some degradation in the cross range resolution.
This paper demonstrates vertical bistatic Radar-Cross-Section measurement capability in the McDonnell Douglas Technologies, Inc. (MDTI) Radar Measurement Center )RMC). Data will be presented showing the system configuration, system specifications, and predicted and measured vertical bistatic RCF data on a variety of generic targets.
Data collection for Synthetic Aperture Radar (SAR) antenna measurements is increasingly making measurement stages very time consuming. This paper presents the capabilities of fast Planar Near Field (PNF) instruments using a linear modulated probe array. It demonstrates the possibilities to decrease the classical near field mechanical scan time by a factor ranging from 100 to 1000. Emphasis is given to the advantages of this technique for multi parameter antenna measurements.
Extracting absolute RCS levels from radar images has become a prevalent practice, but is it valid? Scattering strengths associated with pixels in radar images are derived from responses of the target averaged over frequency and aspect angle. This paper presents theoretical and experimental data for simple and complex targets with frequency-and angle-dependent scattering to illustrate differences between results of narrowband and wideband RCS measurements.
This paper contrasts indoor and outdoor implementation of efforts during upgrades of VHR RCS measurement capabilities. Sites studied are two McDonnell Douglas Technologies Incorporated, Range Measurements Services facilities. Indoor. Radar Measurement Center (San Diego, CA) is a large compact range. Equipment-Harris Corporation Model 1630 Collimator System, Scientific Atlanta Model 2090 radar. Outdoor. Microwave test facility (Victorville, CA), large ground plane facility. Equipment-Steerable dipole feed dish, System Planning Corp, Mark III radar.
The feed support struts often cause noticeable strut lobes in the patterns of reflector antennas. For example, strut lobes are apparent in the measured and calculated patterns presented in Ref. [1] for the 8-foot diameter reflector with a prime focus feed. As pointed out in [1], the calculated strut lobes are higher than the measured ones. The reason for the difference is secondary scattering by the oppositely located strut, which was not modeled in the calculated pattern in [1]. Detailed examination showed a difference of about 2 1/2 dB caused by the secondary scattering for this reflector antenna design. The purpose of this paper is to present measured and calculated patterns which explicitly demonstrate the quantitative effect of the secondary strut scattering. This effort is shown by comparing the measured strut lobe levels with the oppositely located strut removed, i.e., by using 3 struts instead of 4 struts. Calculated patterns are also given in which the secondary scattering is modeled.
Aeronautical SATCOM systems for INMARSAT typically employ circular polarized electronically or mechanically steered multi beam antennas. Characterization of thee antennas requires extensive measurements that differ from conventional antenna pattern measurements. Some of these are: A. Multiple frequently CP gain, axial ratio, and discrimination measurements over a hemisphere for a large number of beams. B. Noise temperature and G/T measurements C. Carrier to multipath rejection D. Intermodulation characteristics E. Receiver and Transmitter system characteristics Details of instrumentation and procedure for these tests are presented with special emphasis on issues such as measurement speed, accuracy and processing of large amounts of data.
This paper discusses a new technology for viewing and measuring the power distribution of a propagating electromagnetic wave. A wave is passed through an absorbing material that absorbs only a small fraction of the energy; the wave is unchanged otherwise. The absorbed energy heats the material so that an engineer can view the power distribution with an infrared camera and get real-time feedback about design changes. Because the engineer is viewing the power distribution of the propagating wave in real-time, normal antenna design schedules are reduce. In agitation, the equipment used in the measurement technique is portable and can be easily calibrated in the field.
A description of antenna measurements performed on an ocean-buoy mounted antenna array is given. The array is designed to measure the E and H fields of a received wavefront at four different heights over the ocean. Four collocated electrically-small loop-dipole antenna pairs at 2 meter height spacings were integrated into a non-conducting buoy support structure. The frequency band was 50-250 MHz. Data was taken with both the Substitution (2-antenna) and 3 Antenna Measurement Methods for comparison purposes. The ground plane range that was used is described as well as the various range setups used to accumulate all of the required data.
The use of electronically scanned phased array antennas in demanding rolls such as satellite communications and radar systems has led to an increasing desire to analyze the sources of error present in the boresight alignment of such systems. Not the least among these errors are those introduced by thermal effects on the various components which comprise the array structure. In an effort to understand this mechanism, this paper will discuss a technique which uses an infrared camera system to analyze the beam deflection errors caused by the effects of temperature gradients present in the antenna system.
The LX/LH organization of McClellan AFB has been using near-field (NF) technology for the past two years to test an Air Force phased array receiving antenna. McClellan uses both a close range surface RF scanner and a larger offset, fain and back-transform near-field scanner. NF testing is done for both trouble-shooting purposes to support repair efforts, and for acceptance-testing to certify the antenna. The purpose of this paper is to show how McClellan interprets its planar near-field data for diagnosing antenna faults. First the various near-field techniques used by the LX/LH organization will be discussed. Following, will be an examination of the antenna defects pointed out by the NF test date. Failures will be traced to the component level where possible. Techniques other than near-field, such as electronic test, will be used to verify these problems. Additionally, the repair methods will be discussed.
Phased array antenna sidelobe levels are evaluated based on the statistics of the differences in element patterns. It is shown that the differences can be treated as random errors. The standard formula for predicting the average sidelobe level of an array due to random errors is valid if the interaction between the element patterns and the excitation function is taken into account. Sidelobes of a linear array with a variety of near-field perturbations are considered. The statistics indicate that for an N-element array, adaptive calibrations may lower the average sidelobe level by a factor of N.
This paper deals with the development of an approach to the design of triad steering antenna arrays which are used in anechoic chambers for hardware-in-the-loop testing of monopulse antenna seeker systems. In the design of a large array, such as those used for hardware-in-the-loop of guided weapons, it is important to optimize the array element spacing. An excessively narrow spacing results in an unreasonable number of required antennas and increased cost, while an excessively wide spacing will induce angle measurement errors in the seeker under test which can be significant. The specific objective of this effort is to quantitatively describe the monopulse discriminant efforts which result when a non-planar field, radiated by an antenna triad, illuminates a monopulse seeker under test. The approach to this problem is to calculate the triad field at the aperture of the monopulse seeker assuming various levels of triad element phase and amplitude error. Using this illumination field and the illumination function of the monopulse antenna, the resulting sum and difference patterns are calculated along with the monopulse discriminant. Software has been developed to perform these calculations. The resulting patterns are compared with the ideal far field pattern and the discriminant bias, or angle measurement error, is quantified.
In this paper, a new error correction technique is introduced to improve the accuracy and efficiency of the traditional NRL Arch method. The use of this integrated technique allows one to correct the error terms in the traditional NRL arch setup so that a broadband evaluation of the performance of the absorber product can be performed with much better accuracy and efficiency. This technique also allows one to conduct large bistatic angle evaluation of absorbers without the cross talk and other error signal interferences. Design guidelines for a broadband NRL test arch are provided so as to successfully implement this improved NRL Arch method for a broadband evaluations of anechoic absorbers. Sample test results from Ray Proof's broadband test arch (0.5-6 GHz) are also presented.
With the recent use of dual-polarized transmission and reception on communications links, the capability to perform accurate polarization measurements is an important requirement of test-range systems. Satellite antennas are commonly measured in the clean, protected environment of compact and near-field ranges, and a circularly polarized feed/field probe is a primary factor in establishing their polarization properties. The feeds also provide excellent source-horn systems for tapered anechoic chambers, where their circular symmetry and decoupling of the fields from the absorber walls improve the often troublesome polarization characteristics of tapered chambers. Circularly polarized feeds are generally composed of four primary waveguide components: the orthomode transducer, quarter-wave polarizer, scalar ring horn, and circular waveguide step transformer. Linearly polarized feeds omit the quarter-wave polarizer. This paper discusses the design and performance of high-polarization-purity source feeds for evaluating the polarization properties of antennas under test. Circularly polarized feeds have been constructed which operate over 10- to 20-percent bandwidths from 1.5 to 70 GHz. Gain values are generally in the area of 12 to 18 dBi, with cross-polarization isolation in excess of 40 dB. Representative measured data are presented.