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A novel system architecture has been developed which makes measurements at N times the analyzer’s frequency, yet requires no communication with the analyzer. Millitech’s Spartan Test Modules, STMs, splits the input signal from an analyzer, multiplies this by N for the source, and by N-1 for the LO of the receiver mixer. The mixer downconverts to the original signal, while maintaining its phase integrity, and sends this back to the analyzer. This scheme is straightforward for narrow bandwidth requirements, but becomes more difficult for wideband ones. The filtering and temperature compensation requirements are high, but have been solved for these bands resulting in a dynamic range of 70 to 80 dB across 54-69 GHz for V-Band and across 69-90 GHz for E-Band, which directly relates to the side lobe resolution in an antenna pattern measurement. The wide dynamic range doesn’t come at a cost of slowing the sweep, as in other frequency extension solutions. This puts the Spartan system performance at the same or higher level as other mixer based systems that have much higher hardware requirements. STMs can be used to convert any make, model or vintage of vector network, scalar network or spectrum analyzer into a millimeter-wave test station. The small size of the STMs allows them to be mounted directly onto the back of the antennas. Therefore, readily available, < 10 GHz cables can be used for the long run back to the analyzer. The Spartan enables state-of-the-art antenna measurements either directly, in compact ranges, or in near-field ranges, examples will be shown.
The Compensated Compact Range (CCR) 75/60 of Airbus DS GmbH is the state-of-the art indoor test facility for real-time RF measurements of satellite antennas within a frequency range from 1 to 200 GHz. The CCR is composed of a two reflector system, a main reflector and a sub-reflector, to create a cross-polar-compensated plane wave in the test zone. However, even such a sophisticated design has residual cross-polar components due to the contribution of the range feed, edge diffraction from the reflector system, as well as from the serrations and imperfect absorbers. To improve and optimize the RF performance of the CCR, detailed EM simulation models are developed in order to solve the related forward scattering problem [1, 2, 3]. In spite of this it is also of great importance to analyze the CCR in a different perspective to gain insight into the CCR. To this aim, an approach based on plane wave spectrum analysis combined with inverse scattering and imaging techniques is proposed. The proposed approach firstly computes the plane wave spectrum of the measured or simulated data taken in the quite zone by using 2D Fast Fourier Transform (FFT). Then, the measured or simulated field is back-propagated by using an inverse scattering approach. By considering the geometrical shape information of the main reflector, the current distribution on the reflector is imaged. The reconstructed images help to clearly identify the effects of. Appropriate windowing is applied to the computed plane wave (angular) spectrum in order to locate and image the echoes. Based on the investigation carried out with the proposed approach, it turns out that the area of the main reflector should be increased to reduce the disturbing impact of the serrations. This investigation also shows that increasing the size of the sub-reflector does not help to improve the plane wave uniformity of the fields in the test zone. In order to test the proposed method against the experimental data, which is not in a suitable format for FFT, the measured data is interpolated to equally spaced data in a Cartesian coordinate system. The experimental results, which are obtained by processing both co and cross polar measurements, show very good agreement with the results obtained by using synthetic data. References [1] A. Geise, J. Migl, J. Hartmann, H-J. Steiner, “Full Wave Simulation of Compensated Compact Ranges at Lower Frequencies”, AMTA 33th Annual Symposium, 16 – 21 October 2011 in Englewood Colorado, USA. [2] C. H. Schmidt, A. Geise, J. Migl, H-J. Steiner, H.-H. Viskum, “A Detailed PO/ PTD GRASP Simulation Model for Compensated Compact Range Analysis with Arbitrarily Shaped Serrations”, AMTA 35th Annual Symphosium, 6 – 11 October 2013 in Colombus Ohio, USA. [3] O. Borries, P. Meincke, E. Jorgensen, C. H. Schmidt, “Design and Validation of Compact Antenna Test Ranges using Computational EM”, AMTA 37th Annual Symphosium , 11 – 16 October 2015 in Long Beach, CA, USA.
Installing a large compact range reflector and electromagnetically qualifying the quiet zone is a major undertaking, especially for very large panelized reflectors. The approach taken to design the required rolled-edge reflector geometry for achieving a 5 meter quiet zone across a frequency range of 350 MHz to 40 GHz was previously presented [1]. The segmentation scheme, fabrication methodology, and intermediate qualification of panels using an NSI-MI developed microwave holography tool were also presented. This reflector has since been installed and the compact range qualified by direct measurement of the electromagnetic fields in the quiet zone using a large field probe. This paper presents the comparison and correlation between the holography predictions and the field probe measurements of the quiet zone. Installation and alignment techniques used for the multiple panel reflector are presented. Available metrology tools have inherent accuracy limitations leading to residual misalignment between the panels. NSI-MI has overcome this limitation by using its holography tool along with existing metrology techniques to predict the field quality in the quiet zone based on surface measurements of the panels. The tool was used to establish go/no-go criteria for panel alignment accuracy achieved on site. Correlation of the holography predictions with actual field probe measurements of the installed reflector validates the application of the holography tool for performance prediction of large, multiple-panel, rolled-edge reflectors. Keywords: Rolled-Edge Reflector, Compact Range, Field-Probing, Quiet Zone, Microwave Holography
Methods for determining the uncertainty in antenna measurements have been previously developed and presented. The IEEE recently published a document [1] that formalizes a methodology for uncertainty analysis of near-field antenna measurements. In contrast, approaches to uncertainty analysis for antenna measurements on a compact range are not covered as well in the literature. Unique features of the compact range measurement technique require a comprehensive approach for uncertainty estimation for the compact range environment. The primary difference between the uncertainty analyses developed for near-field antenna measurements and an uncertainty analysis for a compact range antenna measurement lies in the quality of the incident plane wave illuminating the antenna under test from the compact range reflector. The incident plane wave is non-ideal in amplitude, phase and polarization. The impact of compact range error sources on measurement accuracy has been studied [2,3] and error models have been developed [4,5] to investigate the correlation between incident plane wave quality and the resulting measurement uncertainty. We review and discuss the terms that affect gain and sidelobe uncertainty and present a framework for assessing the uncertainty in compact range antenna measurements including effects of the non-ideal properties of the incident plane wave. An example uncertainty analysis is presented. Keywords: Compact Range, Antenna Measurement Uncertainty, Error Analysis References: 1. IEEE Standard 1720-2012 Recommended Practices for Near-Field Antenna Measurements. 2. Bingh,S.B., et al, “Error Sources in Compact Test Range”, Proceedings of the International Conference on Antenna Technologies ICAT 2005. 3. Bennett, J.C., Farhat, K.S., “Wavefront Quality in Antenna Pattern Measurement: the use of residuals.”, IEEE Proceedings Vol. 134, Pt. H, No. 1, February 1987. 4. Boumans, M., “Compact Range Antenna Measurement Error Model”, Antenna Measurement Techniques Association 1996 5. Wayne, D., Fordham, J.A, Mckenna, J., “Effects of a Non-Ideal Plane Wave on Compact Range Measurements”, Antenna Measurement Techniques Association 2014
Achieving a very large quiet zone across a wide frequency band, in a compact range system, requires a physically large reflector with a suitable surface accuracy. The size of the required reflector dictates attention to several important processes, such as how to manufacture the desired surface across a large area and the practicality of transportation and installation. This inevitably leads to the segmentation of the reflector into multiple panels; which must be fabricated, installed, and aligned to each other to conform to the required geometry. Performance predictions must take into account not only the surface accuracy of the individual panels but also their alignment errors. This paper presents the design approach taken on a recent project for a compact range system utilizing a blended rolled-edge reflector that produces a 5 meter quiet zone across a frequency range of 350 MHz to 40 GHz. It discusses the physical segmentation strategy, the fabrication methodology, the intermediate qualification of panels, the panel alignment technique, and the laser-based metrology methodology employed. Performance analysis approach and results will be presented for the geometry as conceived and then for the realized panelized reflector as machined and aligned.
An uncertainty budget for Indoor Radar Cross Section (RCS) measurements contains many contributors. Typically, one of the largest contributors comes from the Quiet Zone quality. To quantify the ripple and the tapper in the Compact Range Quiet Zone of the CEA’s indoor facility CAMELIA, a diagnosis method has been implemented, exploiting the radar response of a moving sphere located on a polystyrene mast. This polystyrene mast is fixed on the top of a linear-translating table over an azimuth positioner. The combination of the two axis capabilities allows to locate the PEC sphere in a horizontal plane cut of the quiet test zone volume. The other cuts at different altitudes are performed by changing the height of the polystyrene mast. This method samples the magnitude of the illuminating field at fixed spatial points (controlled by a laser tracking) in the Test Zone to determine the magnitude of the ripple and thus the Quiet Zone. These experimental data are then statistically processed to determine the measurement uncertainty at a given frequency. This paper introduces and analyses the results of a measurement campaign dedicated to the characterization of the Quiet Zone of the CEA’s indoor facility CAMELIA.
Compensated Compact Range Facilities are the state-of-the-art RF test facilities for spacecraft payload modules and/or antennas. The outstanding features of the compact range technique are the (a) real-time testing capability, (b) easy to use far-field measurement technique, (c) extremely high frequency capability, (d) end-to-end payload testing at multiple test zones due to scanning features, and last but not least the (e) considerable low cross-polar contribution over the full frequency band between 1 - 200 GHz which is one of the important parameters for telecommunication antenna testing. Upcoming spacecraft antennas with single feed per beam configuration and broadband transponder requirements (up to 500 MHz) need rapid test environments for antenna and payload (end-to-end) measurement campaigns. For the desired wide frequency spectrum the Ka-Band and even higher bands (U, and V) are of interest for the next generation of telecommunication spacecraft antennas. Compensated Compact Ranges provide an excellent test environment for such scenarios. Recent developments for the range feeds up to 200 GHz, a new heavy load and highly accurate specimen positioner design, and the easy enlargeable reflector system within the existing chamber complete the picture of a state-of-the-art test facility for present and future spacecraft testing. The paper will explain the advantages of the selected system design and preferred technology with its resulting features to optimally cover the future requests focusing to new developments in the high frequency range. For typical spacecraft antenna scenarios a comparison between Compact Range and Near-Field facilities will demonstrate the applicability in the frequency range from 1 to 200 GHz. Beside the developed test set-up for the required measurement parameters, typical measurement times and achievable performance with its related error budget will be depicted.
For satellite applications payload measurements are a crucial part of the radio frequency validation campaign before the launch. Parameters like Equivalent Isotropic Radiated Power (EIRP), Input Power Flux Density (IPFD), Gain over Noise Temperature (G/T), Gain over Frequency (G/F), Group Delay, and Passive Intermodulation (PIM) are to be measured in suitable facilities on satellite level. State-of-the-art payload measurements are conducted in compensated compact range facilities which offer a real-time test capability which is easy to setup and use. Closed link tests are straightforward to realize with two compact range feeds employing feed scanning. The measurement techniques as well as the error budgets are well known. Near-field facilities are widely used for antenna pattern measurements. However, there is not much literature available discussing in particular measurements of G/T, G/F, and Group Delay in the near field. Measurements of the above parameters in the near field seem to be feasible, however, the processing of the measured data has to be adapted and further calibration measurements are required. In this paper methodologies for payload parameter measurements in compact range and near field facilities will be described. A comparison of payload measurement campaigns in near field and compact range facilities will be drawn. The techniques will be compared in terms of measurement timing and effort, practicability for satellite applications, and achievable accuracies.
Abstract Antenna far field phase pattern is important for some applications. It can be directly obtained in pattern measurement by far field test range (FFTR) or compact range (CR). However, it is found that the antenna far field phase pattern measured by current near field test range (NFTR) is not correct. For a uniform phase feeding plane array, its far field phase pattern should be near constant in 3dB beam width. However, the antenna phase pattern measured by current NFTR looks square curve vs angle. This paper found out that the root cause of the error is due to different reference planes. Both the amplitude pattern and the phase pattern obtained by current NFTR, in fact, refer to the probe scanner plane, not the antenna plane. This shifting of the reference plane has no effect on amplitude pattern, but has effect on phase pattern. After that, a correction method is proposed. One example is used for the root cause finding and correction technique explanation. According to this paper, if one wants to get phase pattern using NFTR, it is necessary to measure the distance between AUT and probe aperture accurately so as to correct it accurately after measurement and obtain accurate phase pattern.
For future applications telecommunication satellites are built with increasing antenna sizes thus having high demands on the test volumes in antenna measurement facilities. AIRBUS Defence & Space provides highly accurate Compensated Compact Range facilities (CCRs) for antenna and payload testing. Mainly facilities of type CCR 75/60 with a quiet zone of 5 m diameter and facilities of type CCR 120/100 with a quiet zone size of 8 m diameter are installed in various countries. A quiet zone size of 5 m might become a limiting factor for test campaigns of future satellite generations. Since numerous CCR 75/60 facilities are installed worldwide, a quiet zone extension upgrade has been developed which allows enhancing the performance of existing facilities with relatively little effort. Lightweight extension panels are installed on upper and lower edges of sub and main reflector increasing the vertical quiet zone dimension. The possible enlargement of the quiet zone can be optimized to customer needs and is mainly driven by the available chamber dimensions. Besides the extension of the quiet zone dimension also the performance in the existing quiet zone will improve due to the larger reflector surfaces. The cross-polar purity goes down up to -60 dB. The first quiet zone extension upgrade has been recently performed at the facility of Thales Alenia Space in Cannes. The quiet zone has been extended from 5 m to 6 m in the vertical direction. A potential extension of the quiet zone up to 1.8 m has been analyzed and is feasible. The design, installation, and verification of the quiet zone extension will be presented in this paper. Quiet zone probing measurement results in C- and Ku-band will be shown.
Equivalent isotropically radiated power (EIRP) and Saturating flux density (SFD) are two system level parameters often sought during characterizing of spacecraft systems. The EIRP quantity is the power that an isotropic radiator will have to transmit to lead to the same power density that the AUT will effect at a specific angle of interest. A convenient measurement technique is to set up a standard gain antenna as receiver in the far-field of an AUT and to then determine EIRP by measuring the power at the port of the standard gain receiving antenna. Since the distance is known the EIRP can be calculated. SFD is the flux required to saturate the receiver of the antenna under test and is also usually determined on a far-field range. The philosophy of this measurement is to determine the saturation level of the receiver and this is typically achieved by gradually increasing the input power level of the transmitter. This process continues as long as the receiver response linearly tracks the increase in power of the transmitter and is terminated once the receiver is saturated. Thus, SFD can be interpreted as being the receive system parameter analogy of the transmit system parameter EIRP. There is a common misconception that these parameters cannot be measured on a near-field range and that they require far-field (or far-field equivalent, i.e. compact range) conditions for a valid measurement to be made. However, the principles for measuring both of these parameters in a planar near-field range (PNF) were presented in [1]: An EIRP technique is presented in [1] equation 32 and this approach relies on a complex integration of the measured near-field power, the near-field probe gain and a single power measurement at a reference location. A SFD technique is presented in [1] equation 39. This technique also relies on a complex integration of the measured near-field power, the near-field probe gain and a single transmitting probe power measurement at a reference location. Although these descriptions are theoretically concise their execution is not obvious [2] and as a result, there still seems to be hesitation in making (and trusting) these measurements in industry. This paper intends to provide further insight into measuring these two parameters in a PNF range and offers test procedures outlining the steps involved in doing so. The principle goal is to offer further explanation to illuminate the underlying principles. The work presented here is not new, but is presented as a tutorial on this illusive subject. [1] Newell, Ward and McFarlane, “Gain and Power Parameter Measurements Using Planar Near-Field Techniques”, IEE APS Transactions, Vol 36, No. 6, June 1988. [2] Masters & Young, “Automated EIRP measurements on a near-field range”, Antenna Measurement Techniques Association Conference, September 30 - October 3, 1996.
Performance requirements for compact ranges are typically specified as metrics describing the quiet zone's electromagnetic-field quality. The typical metrics are amplitude taper and ripple, phase variation, and cross polarization. Acceptance testing of compact ranges involves phase probing of the quiet zone to confirm that these metrics are within their specified limits. It is expected that if the metrics are met, then measurements of an antenna placed within that quiet zone will have acceptably low uncertainty. However, a literature search on the relationship of these parameters to resultant errors in antenna measurement yields limited published documentation on the subject. Various methods for determining the uncertainty in antenna measurements have been previously developed and presented for far-field and near-field antenna measurements. An uncertainty analysis for a compact range would include, as one of its terms, the quality of the field illuminating on the antenna of interest. In a compact range, the illumination is non-ideal in amplitude, phase and polarization. Error sources such as reflector surface inaccuracies, chamber-induced stray signals, reflector and edge treatment geometry, and instrumentation RF leakage, perturb the illumination from ideal.
Driven by the mobile data communications needs of market broadband antennas at the upper frequency bands are already state-of-the-art, e.g. at the Ka-Band. For the characterization of an antenna the antenna gain is one of the major test parameters. This measurement task is already challenging for standard applications at the Ka-Band. However, for the calibration of remote station antennas utilized in high precision test facilities, e.g. the compact range, even higher measurement accuracies are typically required in order to fulfil the overall system performance within the later test facility. Therefore the requirement for this investigation is to improve the measurement set-up and also the steps to get a failure budget which is better than ± 0.15 dB. Every antenna gain measurement technique is affected by required changes in the measurement setup, e.g. the Device under Test (DUT) or the remote station, respectively. This results for example in a variation of mismatch with resulting measurement errors. To determine and compensate the occurred mismatches, the scattering parameters of the involved components have to be measured and be evaluated with a corresponding correction formula. To quantify the effect for the gain measurement accuracy the remaining uncertainty of the mismatch correction values is examined. Another distortion is caused by multiple reflections between the antenna apertures. To reduce this error source, four additional measurements each with a decreased free space distance should be performed. In addition to the common methods, this paper explains in detail an advanced error correction method by using the singular value decomposition (SVD) and compares this to the standard mean value approach. Finally the restricted distance between both antennas within the applied anechoic far-field test chamber has to be analysed very critically and optionally corrected for the far-field gain at an infinite distance in case the measurement distance is fulfilling the minimum distance requirement, only. The paper will discuss all major error contributions addressed above, show correction approaches and verify these algorithms with exemplary gain measurements in comparison to the expected figures.
?A wide band open boundary quad-ridge horn is investigated to provide multi-octave bandwidth operation for a dual reflector compact range. A commercial off-the-shelf (COTS) multi-octave RF feed was selected and optimized to the existing sub-reflectors. The selection requirements of the COTS multi-octave RF Feed are first determined from a geometric optic (GO) analysis method. These results are used to provide an upper bound of the feed directivity affecting target quiet zone (QZ) performance. Physical Optic (PO) and Physical Theory of Diffraction (PTD) analysis that includes the reflectors serrations are then performed to derive the feed requirements to best meet the QZ specifications. This paper presents the use of COTS multi-band RF feed in a compact range that is properly optimized to the sub-reflectors providing frequency bandwidth to meet QZ performance specifications. Comparisons of these analysis to the QZ field probe measurements of the compact range QZ amplitude ripple phase and scan size comparisons are made to verify the compact range COTS RF feed selection. A multi-octave band RF feed in a compact range application enables highly accurate and efficient test measurement capability for characterization of active arrays over a wide bandwidth in real time.
There are many methods of aligning feeds on a dual cylindrical parabolic sub-reflector compact range. Presented in this paper is a laser tracker and Field probe method that was used to align the RF feed to the sub-reflectors. The laser tracker provides real time positional error measurements that are mapped and these results are used to fine tune the alignment of RF feed to the phase centers of the dual cylindrical parabolic sub-reflectors. Field probe test scans are performed to verify QZ performance of various alignment positions measured comparing scans of amplitude, phase and taper. The laser tracker alignment method provides an efficient and a highly accurate method to achieving precision alignment of the RF feed to the sub-reflector system installed into the dual reflector compact range. High accuracy antenna measurements in a compact range require precision alignment of the RF feed to the sub-reflectors phase center. The quality and size of the RF plane wave field of the quiet zone (QZ) performance is affected by the alignment of the RF feed and sub-reflector system combination. This alignment is accomplished through mechanical adjustments of the x-y-z axis RF feed positioning system. Measurements of both mechanical and electrical bore site is performed and compared across the full measurement spectrum to verify the compact antenna test range (CATR) system positioning accuracy.
Experimental measurement plays a key role for technology maturation in an R&D environment. In this paper we highlight the versatility of a new compact range at the Air Force Research Laboratory (AFRL), Sensors Directorate. In its first year of operation, the OneRY Range supported a wide variety of projects ranging from electrically small antennas to 20’ structures, spanning frequencies of 400 MHz to 45 GHz, and involving applications covering land, airborne, and space-based platforms. Here we present measured results from three different antenna development efforts for the Air Force. The first effort involves a UHF meta-material inspired antenna developed for an airborne application. In addition to successfully demonstrating relatively low frequency capability for a compact range, this effort met the challenge to measure antenna patterns from a physically large target. Results from OneRY are compared to those collected from a tapered chamber. Next we show experimental measurement of digital beam forming (DBF) in a large conformal phased array antenna operating at L and S bands. The DBF experimental testing is part of a follow-on effort to an Advance Technology Demonstration conformal array supporting satellite tracking, telemetry and command (TT&C). Finally, we present results from a “quick look” investigation into the operability of a COTS antenna system matched to a third party radome. The project supports airborne satellite communications at K, Ka, and Q bands. Performance of a high frequency extension (18-50 GHz) to the compact range is examined to include an inter-range comparison to planar near-field measurements. A description of the OneRY Indoor Range is also provided.
In Compact Antenna Test Range (CATR) applications, better cross polar discrimination is often the main motivation for choosing the more complex and expensive compensated dual reflector system as opposed to the simpler and cheaper single reflector system. Other than reflector geometry adjustment, different options have been presented in the literature to improve the cross polar performance of the single reflector CATR [1-4]. One solution is the insertion of a polarization selective grid between the feed and the reflector. The shape of the grids curved strip geometry is determined from the geometry of the reflector and each polarization has a different shape. This approach has been demonstrated to provide Quit Zone (QZ) cross polar performances similar to the dual reflector system on a decade bandwidth. The drawback of this solution is that orthogonal polarizations components cannot be measured simultaneously since a different polarizer grid is required for each polarization [1-2]. Other techniques aim at improving both amplitude/phase taper and cross polarization are based on measurement post processing. Processing techniques have been proposed based on numerical modelling of the range [3] or by de-convoluting the measured pattern with a predetermined range response based on QZ probing [4]. The drawback of these methods are the finite accuracy of the post processing, increased measurement complexity and the difficulty to measure active antenna systems. Recently, the application of conjugated matched feeds for reflector systems aimed at cross polar reduction in space application have received attention in the literature [5-10]. Recognizing, that the cross polar contribution induced by the offset reflector geometry has a focal plane distribution very similar to the higher order modes in feed horns, various techniques have been devised to excite compensating feed modes. Although a very elegant technique, the achievable bandwidth is limited and only single polarized solutions have been presented. A different concept of conjugated matched excitation, overcoming the dual polarization limitation has been introduced in [11-12] based on a patch array feed system. However, this implementation is aimed at applications with different beam-width in the principle planes. In this paper we will introduce a new feed horn concept, based on conjugate matched feeding, aiming at cross polar cancellation in single reflectors CATR systems. The proposed feed system is dual polarized and has an operational bandwidth of 1:1.5. The feed concept is introduced and the demonstrator hardware described. The target QZ <40dB cross polar discrimination is demonstrated by QZ probing of a standard single reflector CATR. References: [1] C. Dragone, "New grids for improved polarization diplexing of microwaves in reflector antennas," Antennas and Propagation, IEEE Transactions on , vol.26, no.3, pp.459-463, May 1978 [2] M.A.J. Griendt, V.J. Vokurka, “Polarization grids for applications in compact antenna test ranges”, 15th Annual Antenna Measurement Techniques Association Symposium, AMTA, October 1993, Dallas, Texas [3] W. D. Burnside, I. J. Gupta, "A method to remove GO taper and cross-polarization errors from compact range scattering measurements," ANTENNAS AND PROPAGATION SOCIETY INTERNATIONAL SYMPOSIUM (APSURSI), June 1989, San Jose, California [4] D. N. Black and E. B. Joy, “Test zone eld compensation,” IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, vol. 43, no. 4, pp. 362–368, Apr. 1995. [5] K. K. Shee, and W. T. Smith, “Optimizing Multimode Horn Feed Arrays for Offset Reflector Antennas Using a Constrained Minimization Algorithm to Reduce Cross Polarization”, IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, VOL. 45, No. 12, December 1997, pp. 1883-1885. [6] S. B. Sharma, D. Pujara, Member, S. B. Chakrabarty,r. Dey, "Cross-Polarization Cancellation in an Offset Parabolic Reflector Antenna Using a Corrugated Matched Feed", IEEE ANTENNAS AND WIRELESS PROPAGATION LETTERS, VOL. 8, 2009, pp. 861-864. [7] S. B. Sharma, D. A. Pujara, S. B. Chakrabarty, and V. K. Singh, “Improving the Cross-Polar Performance of an Offset Parabolic Reflector Antenna Using a Rectangular Matched Feed”, IEEE ANTENNAS AND WIRELESS PROPAGATION LETTERS, VOL. 8, 2009, pp. 513-516. [8] S. K. Sharma, and A. Tuteja, “Investigations on a triple mode waveguide horn capable of providing scanned radiation patterns”, ANTENNAS AND PROPAGATION SOCIETY INTERNATIONAL SYMPOSIUM (APSURSI), July 11-17, 2010 [9] K. Bahadori, and Y. Rahmat-Samii, “Tri-Mode Horn Feeds Revisited: Cross-Pol Reduction in Compact Offset Reflector Antennas”, IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, VOL. 57, No. 9, September 2009. [10] Z. Allahgholi Pour, and L. Shafai, “A Simplified Feed Model for Investigating the Cross Polarization Reduction in Circular- and Elliptical-Rim Offset Reflector Antennas”, IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, VOL. 60, No. 3, March 2012, pp. 1261-1268. [11] R. Mizzoni, G. Orlando, and P. Valle, “Unfurlable Reflector SAR Antenna at P-Band”, Proc. of EuCAP 2009, Berlin, Germany. [12] P. Valle, G. Orlando, R. Mizzoni, F. Heliere, K. van ’t Klooster, “P-Band Feedarray for BIOMASS”, Proc. of EuCAP 2012, Prague, Czech Republic.
In this paper the inverse-source technique or source reconstruction technique has been applied as diagnostic tool to determine the complex excitation at sub array and single element level of a measured array antenna [1-5]. The inverse-source technique, implemented in the commercially available tool “INSIGHT” [5], allows to compute equivalent electric and magnetic currents providing exclusive diagnostic information about the measured antenna. By additional processing of the equivalent currents the user can gain insight to the realized excitation law at single element and sub-array level to identify possible errors. The array investigated in this paper is intended as part of the European Navigation System GALILEO and is a pre-development model flying on the In-Orbit Validation Element the GIOVE-B satellite. The antenna, developed by EADS-CASA Espacio, consists of 42 patch elements, divided into six sectors and is fed by a two level beam forming network (BFN). The BFN provide complex excitation coefficients of each array element to obtain the desired iso-flux shaped beam pattern [6-7]. The measurements have been performed in the new hybrid (Near Field and Compact Range) facility in the ESTEC CPTR as part of the installation and validation procedure [8]. The investigation has been performed without any prior information of the array and intended excitation. The input data for the analysis is the measured spherical NF data and the array topology and reference coordinate system. References [1] J. L. Araque Quijano, G. Vecchi. Improved accuracy source reconstruction on arbitrary 3-D surfaces. Antennas and Wireless Propagation Letters, IEEE, 8:1046–1049, 2009. [2] L. Scialacqua, F. Saccardi, L. J. Foged, J. L. Araque Quijano, G. Vecchi, M. Sabbadini, “Practical Application of the Equivalent Source Method as an Antenna Diagnostics Tool”, AMTA Symposium, October 2011, Englewood, Colorado, USA [3] J. L. Araque Quijano, L. Scialacqua, J. Zackrisson, L. J. Foged, M. Sabbadini, G. Vecchi “Suppression of undesired radiated fields based on equivalent currents reconstruction from measured data”, IEEE Antenna and wireless propagation letters, vol. 10, 2011 p314-317. [4] L. J. Foged, L. Scialacqua, F. Mioc,F. Saccardi, P. O. Iversen, L. Shmidov, R. Braun, J. L. Araque Quijano, G. Vecchi " Echo Suppresion by Spatial Filtering Techniques in Advanced Planar and Spherical NF Antenna Measurements ", AMTA Symposium, October 2012, Seattle, Washington, USA [5] http://www.satimo.com/software/insight [6] A. Montesano, F. Monjas, L.E. Cuesta, A. Olea, “GALILEO System Navigation Antenna for Global Positioning”, 28th ESA Antenna Workshop on Space [7] L.S. Drioli, C. Mangenot, “Microwave holography as a diagnostic tools: an application to the galileo navigation antenna”, 30th Annual Antenna Measurement Techniques Association Symposium, AMTA 2008, Boston, Massachusetts November 2008 [8] S. Burgos, M. Boumans, P. O. Iversen, C. Veiglhuber, U. Wagner, P. Miller, “Hybrid test range in the ESTEC compact payload test range”, 35th ESA Antenna Workshop on Antenna and Free Space RF Measurements ESA/ESTEC, The Netherlands, September 2013
Abstract— The National Institute of Standards and Technology (NIST) presents a plan for evaluating and verifying the performance of the refurbished Ft. Huachuca Antenna Test Facility outdoor compact range. This plan was drawn up based upon information supplied to NIST on the intended applications.
MI Technologies has delivered two new state of the art compact range measurement systems and has worked with Panasonic to develop automated test systems that have reduced the test time by more than a factor of 4. The range design includes significant automation, integration with the antenna’s built in up and down converters, and the ranges are reversible.