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Paper discusses the design, optimization and implementation of a Circularly Polarized (CP) microstrip 2 x 2 sequentially rotated phased antenna array for an X-band onboard satellite transceiver. In the final design, CP radiation is constructed by using CP elements, having unique sequential rotation along with sequential phase shift feeding–giving wider 3dB Axial Ratio (AR) Bandwidth. CP in each patch element is achieved by a perturbation segment, in this case a pair of truncated corners and with a single point feed–reducing complexity, weight and RF loss of the array feed. First analysis based on cavity model approach for the single CP patch is carried out, which is used to determine the normalized perturbation parameter. The initial dimensions are calculated using perturbation analysis. Optimization initially for individual patch and then for the array is performed using full wave analysis tools based on Method of Moments (MoM), and verified using Finite Difference Time Domain (FDTD). Finally, the measured input impedance and radiation patterns are correlated with the calculated results. It is observed that the measured Gain and 3db Beamwidth agrees well with the simulated results of the array optimized using MoM, while the measured results of Axial Ratio, VSWR and reflection coefficients Sxx follows closely the results from the simulations based on FDTD.
High frequency (up through X-band) magnetic materials are gaining in importance across a wide range of applications such as microwave components, electromagnetic shielding, and antenna substrates. Development of new magnetic materials and alloys requires convenient and accurate measurement methods with well-understood uncertainties. For this reason, a finite difference time domain (FDTD) model was developed of a shorted microstrip (single coil) permeameter, appropriate for measuring small samples or thin films. Simulating the response to various magnetic materials, this model was used to analyze the prevailing semi-empirical inversion methods and a new, more accurate inversion method was developed to correct deficiencies in existing techniques.
This paper presents a novel method to evaluate very small stray signals in compact range. The ripples of signals probed by an omni-directional antenna along the orthogonal direction of the bore sight could be treated as signals in time domain. Transforming the probed data with fast Fourier transform (FFT), the direction and amplitude (relative to the test signal) of each stray signal could be obtained. To improve the accuracy, time domain software gating should also be used in calibrating the measurement error of amplitude and phase. The presented method has the ability to measure very small stray signals with good angle resolution. The method has been tested by both simulation using MATLAB and experiment in the compensated compact range CCR120/100 in CAST using a monopole antenna centered on a circular ground plane as a probe. Good results were obtained.
A full time domain characterization bench is realized in the CEA-LETI-Minatec anechoic chamber, to automatically derivate UWB antennas transfer function from waveform acquired by a fast sampling oscilloscope. Time domain measurement technique brings several advantages: faster and simpler measurements, out of band antenna behavior, intrinsic time windowing… Several time domain performance criteria are processed. A comparative method takes into account distortion due to the pulse generator and the test bench. Two different bands 0.3-2 GHz and 2-12 GHz are available. The comparison between frequency and time domain measurements shows excellent results (less than 0.3 dB on gain and 1° on phase) on the 2-12 GHz frequency band. Limitations of the proposed method are also addressed. The dynamic range is better than 35 dB thanks to averaging. Minimum bandwidth limit is evaluated to measure wideband and narrow band antennas.
The dynamic range of a measurement system is typically evaluated in the frequency domain. However, for radar-cross-section (RCS) measurements, time processing of the frequency-domain data is often utilized to determine the temporal or spatial (down-range) location of responses. Dynamic range in the time domain is thus of considerable importance in determining what range of responses can be resolved and identified. While the coherent integration inherent in the pulse-compression process can increase the time-domain dynamic range beyond that of the frequency-domain, non-linearity in the measurement system leads to signal-dependent noise which, in turn, limits the time-domain dynamic range to a much smaller value. Thus, specification and characterization of time-domain dynamic range is critical for understanding the linearity requirements and the time-domain capability of the measurement system. This paper reviews design considerations, error sources, and measurement methods relevant to optimizing dynamic range in the time domain. Examples of time-domain measurements are included.
This paper discusses the process of optimization of a spherical near-field range for measurement of large UHF antennas used in space applications. Results of a study undertaken to understand and optimize range performance in presence of multi-path errors and mutual coupling are presented. Data is presented showing variation in measured patterns of a generic UHF antenna as a function various parameters such as a) use of probes of different gains, b) separation distance between the probe and the antenna and c) absorber rearrangement. Use and effectiveness of software post processing approaches such as spherical mode filtering, time domain gating and use of proprietary algorithms (e.g. “MARS processing” developed by NSI Inc.) is illustrated. Practical implementation of these approaches and corresponding impact on data density, test duration and computational effort are also discussed.
A common apparatus for microwave characterization of intrinsic material properties is the coaxial airline. Often the largest source of measurement uncertainty in the coaxial airline is from air-gaps between the sample and fixture. Previous analyses of air-gaps in these fixtures have been restricted to analytical quasi-static approximations that assume very small air-gaps. In this work, finite difference time domain (FDTD) simulations were used to study the systematic error caused by air-gaps in coaxial airline measurements of dielectric permittivity. The fundamental mode in a coaxial airline is a circularly symmetric TEM wave. Thus body of revolution (BOR) symmetry was assumed, reducing the required computational effort. Comparison of two-dimensional BOR-FDTD to three-dimensional FDTD showed excellent agreement. BOR simulations were conducted for a variety of gap sizes and sample permittivities to catalogue systematic ‘measurement error’. The quasi-static gap models were evaluated with these simulations, showing that traditional corrections are effective only with small gaps and low to moderate permittivity. The conventional wisdom for non-magnetic samples is that dielectric inversion from the transmission coefficient is the most accurate. The transmission-only inversion was compared to the Nicolson-Ross-Weir algorithm, showing that the opposite may be true – that inversion of dielectric properties from both transmission and reflection can be more accurate when gaps are present.
Microwave microscopes that measure surface impedance or roughness have been demonstrated with fine spatial resolutions of less than a micron. These microwave probes are practical only for samples less than a few inches in size. However, composite materials in applications such as multi-layer radomes, embedded frequency selective surfaces, or integrated EMI shielding, have larger length-scale features embedded within a multilayer laminate. Diagnosing larger-scale, subsurface features such as joints/seams, periodic elements, imperfections, or damage is driving a need for methods to characterize embedded electromagnetic properties at mm or cm length-scales. In this research, finite difference time domain (FDTD) simulations and experimental measurements were used to investigate a probe technique for measuring sub-wavelength sized features embedded within a dielectric composite. For these applications, the probe interacted with the sample material via both evanescent and radiating fields. A dielectrically loaded, reduced size, X-band waveguide probe was designed in a resonant configuration for improved sensitivity. Experimental measurements demonstrated that the probe could characterize small gaps in ground planes embedded within a dielectric laminate. Simulations also demonstrated the possibility of detecting more subtle imperfections such as air voids.
This paper describes the method and hardware implementation of a test bed that was designed and built to characterize the reflection characteristics of various types of reflector materials. The system described measures reflection amplitude and phase from flat test panels relative to a metal panel standard at normal incidence and for dual linear polarizations simultaneously. The measurement’s theoretical concept is based on a focused free space technique with time domain gating to remove the effect of multi-path coupling between the test panel and the feed assembly. The system as a whole demonstrates a novel method for measuring the reflection from reflector materials and characterizing their potential impact on polarization purity. The measurement system consists of: 1) A fixed reflector, 2) An alignment fixture accommodating feed assemblies, which include corrugated horns that operate over a 40% bandwidth that may be swapped out in order to cover a continuous frequency band from 18 to 75 GHz and Orthomode Transducers (OMT) in order to measure dual linear polarizations simultaneously, 3) An additional alignment fixture for mounting the flat panels under test, and 4) A Vector Network Analyzer (VNA) and computer for data collection and processing. The system is assembled on a bench top and aligned utilizing a Coordinate Measurement Machine (CMM). Sample results demonstrating the measurement of various types of reflector materials including composite reflector lay-ups with graphite face sheets and mesh samples for deployable reflectors are presented.
There is interest in the propagation of EM signals inside jet engine turbines for a number of reasons. Applications include radar scattering phenomenology and jet engine plasma plume formation studies. In our research, we are interested in the communication channel characteristics for micro-size wireless sensors attached to the turbine blades that measure parameters such as strain and temperature. Propagation measurements were performed on both F-16 (F-110) and Boeing 747 (CF6-50) turbines. The frequency band extended from 2 to 20 GHz (wavelengths longer than the turbine blades to wavelengths shorter than the gap between turbine blades). Signals were propagated with both radial and circumferential polarization. Both transmission and scattering measurements were made from both the inlet and the outlet. We also used small probe antennas inserted in boreholes between turbine stages. A range of blade positions were included. We will show the propagation characteristics as a function of polarization, frequency and time (UWB time domain transformations). We will also show the internal radar reflection characteristics of the turbine as a function of various stator blade rotation angles. Comparisons with a hybrid mathematical propagation model will be given.
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 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.
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.
A low-profile, high efficiency sixteen-element stacked patch microstrip array operating in the L-band frequencies of 1.26GHz and 1.413GHz was designed, fabricated and tested for use in applications to airborne sensors operating on small aircrafts. The array was optimized for element spacing, excitation amplitude taper, low cross-polarization and high beam-efficiency using Particle-Swarm Optimization (PSO) and Finite-Difference Time Domain (FDTD) methods. The design and measurement of sixteen-element array topology, stacked patch elements, and power-divider beam forming network are presented in detail. The study highlights the repeatability measurements and characterization of array with the effect of dielectric radomes in a spherical near-field test facility at UCLA. The results met the requirements of center-frequencies and frequencybands(1.26GHz ± 10MHz, 1.413GHz ± 15MHz), side-lobes, very good beam-efficiency (>90%) and low-cross polarization (<-40dB) in main-beam region of array. The measured results compared well with simulations for the two frequencies. Based on measurement results, the microstrip array design has a potential to be used as a feed for deployable mesh antennas for future spaceborne L-band passive and active sensing systems that can operate at integrated active radar (1.26GHz) and passive radiometer (1.413GHz) frequencies with dual polarization capabilities to study soil-moisture and sea-surface salinity.
This paper presents a Radar Crossed Section (RCS) time-domain near-field measurement and its Inverse Synthetic Aperture Radar (ISAR) imaging. The target includes a pyramidal horn and a metallic aircraft scale model. A pulse generator excites the transmit antenna and a digital sampling unit collects the data at the receiving side. A time gating window is subsequently applied to reject the multiple reflections. An efficient 3-D algorithm for ISAR based on time-domain near-field data is presented. The test results for six cases demonstrate excellent ISAR images. In particular the geometry of 3-D reconstructed target can be displayed in perspective manner. The advantage of using time-domain near-field measurements is three-fold. First, it reduces measurement time in the order of one-tenth compared to frequency-domain measurements. Second, it mitigates the multiple reflection effects via time gating. Third, near-field measurements require relatively little real estate which reduces the cost tremendously since a compact range is not needed.
This paper presents a novel variable width time gating technique, which is applied to planar and cylindrical near-field data in impulse time-domain antenna near-field measurements. Due to the changing distance between the probe and the antenna under test (AUT) in planar and cylindrical scans, the conventional fixed time gating technique causes problems to remove multiple reflections from the desired AUT response. It further limits the application of time-domain measurement to planar and cylindrical scans. The new variable width time gating technique provides a flexible way to solve these problems. Test results for both planar and cylindrical near-field measurements are presented. The difference of far-field patterns between time-domain and frequency-domain near-field measurements is noticeable. We also show the effects on the far field patterns due to fixed and variable time gating windows. We further conclude that the time-domain technique also works for planar and cylindrical near-field measurements by using variable width time gating technique.
Compact antenna test ranges such as the ESA/ESTEC CPTR are large facilities for the characterization of electrically and physically large antennas as well as end to end radiated payload testing. To achieve high accuracy measurements, time gating is used to filter out as many room effects as possible. The most common implementation of time gating is to perform a frequency sweep, Fourier transformation to the time domain followed by windowing, gating and back transformation to the frequency domain. All of this is at a time penalty. An alternative is to have a synchronised switching system to switch on and off the transmit power as well as switching on and off the receiver. Such a solution has been devised in a cooperative effort between EADS Astrium and the Munich University of Applied Sciences. The paper will present the capabilities of the Astrium HG2000 Hard Gate system (1) in the ESA/ESTEC CPTR, its implementation in the facility as well as presenting direct comparison of results obtained by the hard gate system with the conventional soft gate on both low gain and high gain antennas
We characterize here the performance of a time domain antenna range by measuring a number of antennas, comparing the results to frequency domain measurements. Our time domain antenna range consists of a fast pulser and a sampling oscilloscope. We have demonstrated good performance of this range for all types of antennas (resonant and non-resonant) that operate between 900 MHz and 20 GHz. Furthermore, if the antenna is non-resonant, then good performance is observed as low as 200 MHz. Finally, it seems likely that by using a longer time window we can extend below 900 MHz the bandwidth of the antenna range for resonant antennas.
Spectrum is presently one of the most valuable goods worldwide as the demand is permanently increasing and it can be traded only locally. The United States FCC has opened the spectrum from 3.1 GHz to 10.6 GHz, i.e. a bandwidth of 7.5 GHz, for unlicensed use with up to -41.25 dBm/MHz EIRP. Numerous applications in communications and sensor areas are showing up now. Like all wireless devices these devices have an antenna as integral part of the air interface. The antennas are modeled as linear time invariant (LTI) systems with a transfer function. The measurement of the antenna’s frequency dependent directional transfer function is described. Furthermore the measured transfer function is transformed into time domain, where it is used to characterize pulseshaping properties of the antennas. Additionally, measurements in time domain, which were performed with a pico-second pulse generator and a 50 GHz sampling oscilloscope, are presented and compared to the transformed frequency domain measurements. These measurements enable the realistic characterization of ultra wideband antennas for UWB link level simulations.
Over the last decade there has been great interest in ultrawideband (UWB) communication systems. Ultrawideband antennas that are able to transmit or receive short pulses with no distortion are called Impulse Radiating Antennas (IRA). One of the most commonly used IRA.s consists of a parabolic reflector fed by conical transmission lines that propagate a spherical TEM wave. The reflector IRA was constructed, analyzed and measured at UCLA. A method of moments based software, Hybrid EFIE and MFIE Iterative (HEMI), is employed to simulate the antenna. The software has to be run many times for a wide frequency range. The simulation results for the current distribution on the conical coplanar feeds show that one of the arms can be used as an UWB balun and the unbalanced line can be connected to the antenna. The aperture field is studied by calculating the surface current on the reflector. These current distributions show that the aperture field is tapered from edge to center and the center part is less illuminated in comparison with the edges. This increases the side lobe level for reflector IRA. To measure the time domain characteristics of an IRA, we have to use either short pulses and a time-domain setup or many frequencies in a wide frequency band and use an inverse Fourier transformation to calculate the time-domain results. In this work, we used frequency domain measurement setup to measure the antenna characteristics. The recently constructed spherical near-field measurement chamber at UCLA is used to measure the radiation characteristics of the antenna. The far-field calculated from the near-field measured data is compared with the HEMI results. Calculated and measured results show good agreement.