Browse Topic: Antennas

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This SAE Aerospace Recommended Practice outlines a standardized and economical method for the checkout and calibration of electromagnetic interference measurement antennas. Its application is for use when measuring a source 1 m from the antenna in a shield room. This is the typical distance used in performing military EMC testing. The influence of the shield room on the measured field strength is not considered. This standard does not address the measurement of emissions from an unknown distributed source, yet it attempts to resemble reality by using another antenna, in the calibration method, that represents a distributed source. This document presents a technique to determine antenna factors for antennas used primarily in performing measurements in accordance with References 2.1 and 2.2. The purpose of Revision B was to include the calibration of other antennas, such as biconical, horn, monopole and small loop antennas that are also specified for use in these same references. Revision D includes a specific procedure for loop antennas that are separated by 1 m from the device under test. Revision E adds the inclusion of modern instrumentation, instruction on how to calibrate the hybrid antenna, and attempts to improve upon the clarity of this document for the user.
AE-4 Electromagnetic Compatibility (EMC) Committee
The antennas number is increasing on-board rotorcraft and this trend is not ready to slow down regarding the growing need of connectivity. Rotorcrafts, especially the lightest ones will soon be saturated in antennas. This paper, without being exhaustive, presents some ways to tackle this fact, with the use of integrated antennas. Besides technical difficulties, the current certification constraints should be re-defined or at least adjusted.
DUTRUC, HerveFilias, François-Xavier
ABSTRACT The US Army's Aviation Development Directorate (ADD) has successfully collaborated with its industry partners to reduce system parasitic weight for aviation platforms through multifunctional structures technology development. In short, this can be generalized as achieving weight savings by replacing the combination of aircraft structure and an independent, add-on mission enabler with a singular system that performs the functions of both structure and mission enabler. This extensive multifunctional technology development for aviation structural applications has yielded significant weight savings over parasitic designs. Technologies demonstrating this structural multifunctionality for weight reduction include integrally armored helicopter floor, lightweight integrally armored helicopter floor, lightning-protected structure, structural antenna aperture, helicopter empennage antenna structure, combat tempered aft fuselage, blast attenuating aircraft structure, and highly durable floor armor for rotorcraft. The significance of weight savings that can be enabled via multifunctional structures technology development is clear. One case study exercise indicates a platform-level mission enabler weight savings of 17.8%. This significance of weight savings is analogous to other studies showing synergistic benefits from technology integration at the technology and system (platform) level.
Robeson, Mark
Prediction Method for Automobile EMI Test Result in AM Frequency Band *CSP Meta QA Testing*2017-01-00143/28/2017
The EMI, electromagnetic interference, is tested for automobiles and components by the method defined in the international standard, CISPR 25. Regarding the automobile test, the EMI from the component installed in the automobile is measured by the antenna of an automobile. On the other hand on the component test, the EMI from the component is measured by a mono-pole antenna set forward of the component. However, components sometimes fail the automobile test even if its passed the component test due to the difference of the method. In this case, the component has to be designed again to pass the automobile test. Therefore, the prediction method of the automobile test result is required. In this paper, we tried to modify the standard component test configuration to predict the automobile test result for a fuel pump system in AM frequency band. At first, to show the noise propagation mechanism of the automobile test, the mechanism was modeled by an electrical circuit by focusing on the parasitic capacitances between the fuel pump system, the antenna and the chassis. Next, to realize the same electrical circuit as the automobile, the standard component test configuration was modified. For example, in the standard component test, the fuel pump should be set on the grounded ground plane. On the other hand, in the modified component test, the fuel pump was set between the floor and floating ground plane. As the result, the modified component test result agreed with the automobile test result, meaning automobile test result could be predicted.
Nomura, TakashiKawai, Kazuma
3D Automotive Millimeter-Wave Radar with Two-Dimensional Electronic Scanning2017-01-00473/28/2017
The radar-based advanced driver assistance systems (ADAS) like autonomous emergency braking (AEB) and forward collision warning (FCW) can reduce accidents, so as to make vehicles, drivers and pedestrians safer. For active safety, automotive millimeter-wave radar is an indispensable role in the automotive environmental sensing system since it can work effectively regardless of the bad weather while the camera fails. One crucial task of the automotive radar is to detect and distinguish some objects close to each other precisely with the increasingly complex of the road condition. Nowadays almost all the automotive radar products work in bidimensional area where just the range and azimuth can be measured. However, sometimes in their field of view it is not easy for them to differentiate some objects, like the car, the manhole covers and the guide board, when they align with each other in vertical direction. In other words, those objects are counted as one erroneously because of absence of height information. In practice, road conditions are complicated and unpredictable, these unexpected mistakes will make the ADAS poor performance or even collapse, e.g. unwanted abrupt brake due to the detected manhole cover or guide board. Plus, the subsequent target tracking would be made an arduous task and with untrusted output. This paper proposes an automotive radar architecture with two-dimensional electronic scanning, which can obtain 3D information--range, azimuth and height. Four antennas including one transmitting antenna and three receiving antennas are used in this scheme. In addition to two conventional receiving antennas placed in horizon, another receiving antenna is arranged in vertical aligning with one of the other two to obtain the height information so that the corresponding detected targets can be distinguished clearly. Furthermore, when more antennas utilized this architecture can be extended easily for higher autonomous driving requirements. A range of simulation indicates that this radar architecture can measure object height and the effectiveness of proposed architecture is further verified in actual experiments on the corresponding radar prototype. It is low-cost and with small size, and the car grade design and development make the further application in ADAS possible.
Bai, JieCHEN, SihanCui, HuaBi, XinHuang, Libo
Many modern aircraft, including rotorcraft, require conformal antennas and fairings to reduce wind drag, ice accretion, lightning strikes, and impact damage. An innovative composite wing configuration with a structural Ultra High Frequency (UHF) antenna window "aperture" has been developed. The wing is based on variants of lightweight X-Cor® sandwich core technology for durability and damage tolerance, with tailored electromagnetic properties in the aperture region of the wing. This paper presents a brief introduction to helicopter wings, a summary of recent research at Boeing and Army leading to this design, and the development approach used for this project. Structural and electromagnetic analyses are provided, and measurement results of an early prototype are summarized. The emphasis of this paper is on the wing configuration details surrounding the antenna aperture. The approach can be replicated on almost any current or future aircraft or rotorcraft.
Tyrell, StaceyRobeson, MarkKube, CourtneyMcCarthy, DennisLavin, Ronald
Development and Application of FM Multipath Distortion Rate Measurement System Using a Fading Emulator Based on Two-Stage Method2016-01-00824/5/2016
The suitability of FM radio receivers for automobiles has conventionally been rated by evaluating reception characteristics for broadcast waves in repeated driving tests in specific test environments. The evaluation of sound quality has relied on the auditory judgment due to difficulties to conduct quantitative evaluations by experiments. Thus the method had issues in terms of the reproducibility and objectivity of the evaluations. To address these issues, a two-stage method generating a virtual radio wave environment on a PC was developed. The research further defined the multipath distortion rate, MDr, as an index for the sound quality evaluation of FM receivers, and the findings concerning the suitability of the evaluation of FM terminals for automobiles were reported at the 2015 SAE World Congress. However, extended periods of measurement were necessary because the upper limit for delay time, τMax, cannot be determine in advance for the measurement of MDr using the Two-Stage Method. This research clarified the characteristics of the multipath distortion rate, MDr, in relation to the modulation frequency (fm) and the delay time (τ) of the FM broadcast wave, and preliminarily determined τMax, the upper limit for delay time necessary for the Two-Stage Method. The research also indicated the possibility of applying the Two-Stage Method to Intelligent Transport Systems (ITS) to evaluate reception in the case of vehicle-to-vehicle communication on PC. By comparison with conventional proving trials, the Two-Stage Method makes it possible to generate radio wave environment characteristics as desired, and represents a useful evaluation tool displaying good reproducibility.
Komatsu, SatoruKarasawa, YoshioKashiwa, TatsuyaTaguchi, KenjiImai, Suguru
Fabrication of an Integrated Photonic Waveguide Joint in Micromachined SiliconTBMG-242554/1/2016
High-aspect-ratio silicon structures are necessary components in many MEMS (microelectromechanical systems). Aspect ratio is defined as the ratio of the height of the structure to its lateral width. The structures are typically fabricated through bulk micromachining steps such as deep reactive ion etching. In some cases, multiple levels of high-aspect-ratio structures are required. For instance, one may want to etch completely through a silicon wafer to thermally isolate a bolometer or provide waveguide coupling to an antenna defined on an insulating membrane, and at the same time have integrated high-topology structures required for microwave coupling or filtering. Definition of the structures typically uses photolithographic technology. But for high-aspect-ratio structures, spin cast resist becomes difficult to incorporate due to the non-uniform thickness of the resist around tall structures. One can cast very thick layers of photoresist, but this limits the minimum feature size, and additionally, very thick layers of photoresist are difficult to work with due to solvent release and moisture that can cause the resist to crack or swell. For electromagnetic reasons, the structures would preferably be made from conductive material such as metal or degeneratively doped silicon. The objective of this work was to incorporate multiple levels of conductive high-aspectratio structures with standard micromachining processes.
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