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Spherical near-field measurements have become a common way to assess performance of a wide variety of antennas. Published reports on range error assessments for spherical near-field ranges however are not very common. This is likely due to the perceived additional complexity of the spherical near-field measurement process as compared to planar or cylindrical measurement techniques. This paper will establish and demonstrate a simple procedure for characterizing the performance of a spherical near-field range. The measurement steps and reporting can be largely automated with careful attention to the test process. We will summarize the process and document the accuracy of a spherical near-field test range at NSI using the same NIST 18 terms commonly used for planar near-field measurements.
The purpose of this paper is to detail the process used to optimize the low frequency performance of 72 inch absorber. The loading optimization was required to provide enhanced performance of a twisted 72 inch absorber which was to be used in the building of a large aircraft test facility. The chamber performance requirements are over a frequency range of 30 MHz to 18 GHz. The chamber dimensions are 30 meters x 30 meters x 20 meters high. This chamber will be used to measure a variety of fighter aircraft for many EW scenarios. The mission of this facility is to “perform radiated immunity testing of aerospace vehicles with high electromagnetic field intensity, radiated emissions measurements, EMC testing, electronic warfare testing, antenna pattern testing”. Due to the broad frequency range and the fact that the chamber is desired to test both in the low frequency EMC domain and high frequency antenna measurements, an extremely broad band absorber material had to be developed and optimized. The use of ferrite hybrids was considered. Due to the roll off at microwave frequencies and the expense of such a high volume of materials, they were eliminated for cost and due to the limited performance in the 1-2 GHz frequency range. The ideal candidate is a 72 inch twisted pyramidal geometry. The standard loading of these materials is ideal for frequencies above 150 MHz.. The performance level in the 30 MHz to 150 MHz range is less than ideal. A design for the chamber was established with specific target performances required of the 72 inch absorbers. This paper describes the effort taken to optimize the loss properties of the dielectric foam to meet the target absorber performance required for the implementation of the design. Key Words: Absorber Measurements, Absorber Performance, Computer Modeling of Absorbers, Dielectric Properties of Absorber
The measurement of the radiation patterns of the PLANCK Radio Frequency Qualification Model (RFQM) is one of the most important elements of the verification of the PLANCK telescope. PLANCK is one of the scientific missions of the European Space Agency and is devoted to observe the Cosmic Microwave Background radiation, with unprecedented accuracy. The satellite payload consists of two state-of-the-art, cryogenically cooled instruments sharing a dual reflector telescope with 1.5 m aperture and covering the frequency range from 27 GHz to 1000 GHz. As a key part of the telescope verification logic, the radiation patterns of the RFQM has been measured in the Alcatel Alenia Space Compact Antenna Test Range (CATR) at four frequencies (30, 70, 100 and 320 GHz) using representative flight feed horns of the focal plane unit. This paper presents the test logic, the measured radiation patterns, the custom-made instrumentation set-up, the correction techniques used and the final link to the Flight Model verification.
This paper describes the new NIST tabletop millimeter-wave extrapolation range that will provide on-axis gain services up to 110 GHz. A discussion of the extrapolation measurement method, as presented at the Antenna Measurements Techniques Association (AMTA) in 1999, is the basis for much this paper. The extrapolation method for determining gain of directive antennas at quasi-near-field distances is based on a generalized three-antenna approach. It has been used at NIST for more than twenty years to calibrate antenna gain standards up to 20 GHz to within 0.1 dB and up to 50 GHz to within 0.15 dB. The basic theory, description of the measurement system, data acquisition procedure, and measurement results for three antennas at 94 GHz will be presented.
Adaptive array based antenna pattern comparison technique is presented in this paper. In the method, the antenna pattern of the antenna under test (AUT) is measured several times at different positions in the quiet-zone. The corrected antenna pattern is obtained by taking a weighted average of the measured patterns. An array synthesis algorithm is used to obtain averaging weights at the different rotation angles of the AUT. In addition, the weights are adapted specifically for the AUT. The adaptive array correction technique is demonstrated in a hologram based compact antenna test range (CATR) at 310 GHz. The demonstration is based partly on the measurements and partly on the simulations. For verification, the accuracy provided by the method is compared to the accuracy provided by the uniform weighting.
The potential transmit power, and hence dynamic range of monostatic millimeter wave RCS measurements may be limited by the feed coupling of the antenna. Time domain gating can be used to reduce the measurement errors caused by this signal, as well as other undesired signals from scattering sources in the range, but does not protect the receiver from compression. Hardware gating can allow increases in transmit power by protecting the receiver from the effects of the feed coupling return. Unfortunately, equipment capable of hardware gating at millimeter wave frequencies is difficult to obtain. In addition, the usefulness of hardware gating is limited by the duty cycle loss in the measured signal. We describe a practical system using gating of the low frequency intermediate frequency (IF) signal in the receiver and a microwave pulse modulator prior to the millimeter wave multiplier in a mono-static millimeter wave RCS measurement system. We also describe methods to minimize the loss of measurement dynamic range due to duty cycle losses in this system. We demonstrate the use of this system for RCS measurements of simple targets, and compare the results with those obtained using software gating alone.
The planar near-field antenna measurement system at KRISS has been upgraded to V-band (50 GHz – 75 GHz). This paper describes the upgraded planar near-field antenna measurement system that consists of a planar near-field scanner, a microwave subsystem and an extrapolation range, and shows the uncertainties in gain for a rectangular near-field probe and a Cassegrain antenna at 65 GHz.
Hand-made scale models in antenna measurements have been used since the late 1940s. Today, aircraft models are fabricated using a stereolithography (SLA) process and the Computer Aid Design (CAD) for manufacturing the full size aircraft. This is the fabrication method used for the V-22 1/15th scale model. Once the SLA machine is programmed, these models are very inexpensive to produce. In this paper, antenna patterns measured on the V-22 scale model are compared with antenna patterns measured on the aircraft in-flight. Comparison of the patterns shows high correlation. Figure 1 V-22 Aircraft
The Phoenix Lander, a NASA Discovery mission which lands on Mars in the spring of 2008, will rely entirely on UHF relay links between it and Mars orbiting assets, (Odyssey and Mars Reconnaissance Orbiter (MRO)), to communicate with the Earth. As with the Mars Exploration Rover (MER) relay system, non directional antennas will be used to provide roughly hemispherical coverage of the Martian sky. Phoenix lander deck object pattern interference and obscuration are significant, and needed to be quantified to answer system level design and operations questions. This paper describes the measurement campaign carried out at the SPAWAR (Space and Naval Warfare Research) Systems Center San Diego (SSC-SD) hemispherical antenna range, using a Phoenix deck mockup and engineering model antennas. One goal of the measurements was to evaluate two analysis tools, the time domain CST, and the moment method WIPL-D software packages. These would subsequently be used to provide pattern analysis for configurations that would be difficult and expensive to model and test on Earth.
Antenna pattern and isolation measurements for the B-1 Fully Integrated Data Link (FIDL) Program have been completed at the US Air Force Research Laboratory (AFRL) Antenna Measurements Facility located near the AFRL Rome Research Site (RRS), Rome, NY. This combined satellite and airborne communications upgrade has been performed under the supervision of the B-1 Systems Group, Wright Patterson AFB, Ohio. One eighth scale antenna patterns were collected on a far field range for new Link-16 antennas, a relocated VHF/UHF2/L-Band antenna and the new Satcom transmit antenna, while on a one eighth scale B-1 model. Antenna to antenna isolation measurements were performed with antennas mounted on a full scale front section of the B-1 airframe. The RF Technology Branch (IFGE) has developed techniques for evaluating the effects of airframe and external stores on the radiation pattern characteristics of antenna systems in a simulated flight environment. Data obtained in this manner is used to evaluate antenna radiation characteristics of antenna/systems without the requirement of an extensive flight test program. Using similar techniques, AFRL has developed procedures whereby precision measurements of isolation between aircraft mounted antennas can be accomplished. This paper will present how the measured data was obtained for the antennas involved in the FIDL upgrade.
Using software and measured receive power data from aircraft during flight test, the pattern of the installed antenna is derived and validated. During the test flight, data packets were continuously transmitted from an aircraft using the antenna under test. The aircraft flew a designated pattern having straight legs oriented at specific angles to the ground station. Throughout each of these legs the aircraft performed appropriate maneuvers to provide elevation pattern data. A ground station recorded the received data packet signal strength with GPS time tags. Position data of aircraft (latitude, longitude, and altitude) and attitude (roll, pitch, and yaw) was recorded with time tags. Satellite Tool Kit, (STK™), by Analytical Graphics Inc. [1] reproduces flight test conditions and calculates the predicted ground station receive power based on vector direction, range, and a theoretical pattern for the antenna under test. The result is a dynamic link budget and a graph plotting predicted received signal strength versus time. Overlaying the recorded ground station received signal strength with the predicted signal strength allows the correlation of the measured data to that calculated using the theoretical antenna pattern. Curves are presented which show correlation sufficient to validate pertinent portions of the theoretical antenna pattern.
The AN/SPS-48E antenna is a three dimensional air search antenna that is currently installed on 27 US ships. Currently the 48E antenna is removed from the ship after five to seven years to be overhauled at NSWC Crane Division. The new San Antonio Class ships (LPD 17 – 25) have a new enclosed mast design, the Advanced Electromagnetic Mast/Sensor (AEM/S), in which the 48E antenna and others are installed inside the enclosed mast. The cost of removing the enclosed mast led to the decision that the 48E antenna systems (antennas and pedestals) will not be removed for overhaul and maintenance on these ships as is currently done for all other installations. As a result, new fixtures and procedures need to be developed to allow maintenance inside of the mast. The most challenging of the new fixtures is a near-field scanner, which will be used to re-tune the antenna and characterize the RF performance parameters. This paper discusses the design and development effort currently underway for this Enclosed Mast Antenna Calibration System (EMACS), most notably the mechanical design constraints placed on the scanner by the enclosed mast regarding equipment movement, installation, alignment and testing.
A wide range of wireless services are being installed in modern vehicles. Applications including radio reception (FM), navigation systems (GPS), satellite radio, keyless entry, future data services (IEEE 802.11) and mobile telephone are increasingly installed in modern vehicles. Integration of these technologies in cars and trucks has generated a need to accurately determine the performances of the antenna devices when mounted on the vehicle.
The groundwave correction method of measuring the gain of a vertical antenna over a lossy ground plane is an accepted means of performing a gain measurement without the need for a standard reference antenna. However, on antenna ranges where the ground plane is not uniform, this approach may not yield accurate results over certain portions of the test band due to discontinuities in the ground. This paper shall present a method for using surface impedance methods to predict the performance of an outdoor antenna test range that has a non-uniform ground. Comparison with measured data shall also be presented over the commercial HF and VHF bands.
Large ground terminal antennas for high data rate applications provide challenges to demonstrate compliance with their specified performance. Such antennas have narrow beamwidths and require evaluation of their antenna tracking performance. Terminal testing is normally performed in vendor acceptance tests that demonstrate the antenna design compliance, site installation tests that evaluate the operational compliance of the “as installed” antenna, and operational testing performed for maintenance and diagnostic purposes. The advantages and limitations of three distinct measurement techniques, radio source, satellite signals of opportunity, and boresight tower measurements are discussed.
Position uncertainty in antenna measurements is unavoidable. This is due in part to mechanical inaccuracy in the fixturing and positioning equipment. For many classes of antenna, there is also not an obvious choice of reference point, due to lack of a well-defined phase center. It has been shown [1] that a UWB transfer function measurement, taken either in the time or frequency domain, is highly sensitive indicator of antenna displacement. Extraction of the linear phase from the transfer function data results in a uniquely defined distance for any given pair of antennas in a given orientation. When a two- or three-antenna measurement using identical antennas is performed, the result is a unique reference plane for the antenna. Unlike the phase center, is not tied to a particular frequency. Here, using frequency domain measurements of monopoles, ridged horns, and an end-fed biconical antenna, we show that distances can be extracted with a high degree of repeatability. Resolution on the order of 1 part in 5,000 can be obtained in a 4-meter chamber with measurements extending to 20 GHz. Thus, variation in the extracted distance should be a highly sensitive indicator of positional inaccuracy.
In antenna measurements, the orientation of the antenna under test (AUT) is very important. The orientation here refers to the antenna placement in a plane perpendicular to the incident wavefront. For a linear polarized antenna, the antenna should be oriented parallel to the co-polarized component of the incident fields. A small error in the orientation can lead to a drop in the measured gain and an increase in the measured cross-polarization level. In the case of a circularly polarized antenna, it is not obvious how the antenna should be oriented. If the quiet zone fields (incident wavefront) have no cross-polarized component, then the orientation does not affect the measured data. However, when the quiet zone fields have a cross-polarized component, which is true for almost all test ranges, the measured gain and cross-polarized level can vary significantly with the antenna orientation. In this paper, the measured data is used to show the effects of antenna orientation on a circularly polarized antenna. The reason for the variations in the measured data with antenna orientation is discussed. A simple method to improve the measurement accuracy is presented.
In the early 1990's, Georgia Tech Research Institute (GTRI) was able to acquire an unclassified phased-array antenna from the former Soviet Union. Since that time, GTRI personnel have analyzed the antenna for design features that enabled the production of low-cost phased-array antennas. Antenna pattern data collected on the GTRI planar near-field range of a working and errored antenna will be presented. Also, modeled antenna pattern data will be presented as a comparison to show the particular effects of the low-cost design versus an ideal antenna. Finally, the original control mechanism of the phased-array antenna will be analyzed and compared with a modern control mechanism developed by GTRI researchers. Control data for the original and new control systems was captured with a logic analyzer and will be presented for comparison.
The time delay behavior of antennas is of high importance for high accuracy localization and navigation systems. Next to the investigation of the receiving antennas, the transmitting antennas are of substantial interest, too. In the application envisioned these antennas are small dipoles integrated in a battery powered miniaturized transmitter system. The method described in this paper is based on the measurement of the time difference of arrival of a broadband signal in a synchronized setup. This setup consists of the transmitter under test which transmits a bursted sequence of the localisation waveform. The receiving side of the measurement system consists of two antennas, where one works as a reference antenna (with fixed position in relation to the transmitter) and the other works as “classical” probe antenna. Two synchronized tuners and data acquisition systems determine the time difference of arrival of the signal. Detailed measurements of different transmitters have been performed in the 2.45 GHz ISM band and will be presented.
The UWB radar operates simultaneously over large bandwidth and the antenna parameters must refer to simultaneous performance over the whole of the bandwidth. Conventional frequency domain (FD) parameters like pattern, gain, etc. are not adequate for UWB antenna. This paper describes an UWB radar antenna planar near field (PNF) measurement system under construction to get the impulse response or transient characteristic of the UWB antenna. Unlike the conventional antenna or RCS time domain test system, the UWB radar signal instead of the carrier-free short time pulse was used to excite the antenna that can avoid the decrease of the dynamic range and satisfy the needs of SAR and the other UWB radar antennas measurement. In order to demonstrate the data analysis program, FDTD simulation software was used to calculate the E-field of M×N points in a fictitious plane at different times just like the actual oscilloscope’s sampling signals in the time domain planar near field (TDPNF) measurement. The calculated results can be considered the actual oscilloscope’s sampling output signals. Through non-direct frequency domain near field to far field transform and direct time domain near field to far field transform, we get the almost same radiation patterns comparing to the FD measurements and software simulation results. At last, varied time windows were used to remove the influences of the non-ideal measurement environment.