2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)最新文献

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Stereoscopic Vision-Based Relative Navigation for Spacecraft Proximity Operations 基于立体视觉的航天器接近操作相对导航
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453524
M. Mazzucato, A. Valmorbida, A. Guzzo, E. Lorenzini
{"title":"Stereoscopic Vision-Based Relative Navigation for Spacecraft Proximity Operations","authors":"M. Mazzucato, A. Valmorbida, A. Guzzo, E. Lorenzini","doi":"10.1109/METROAEROSPACE.2018.8453524","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453524","url":null,"abstract":"The capability of a spacecraft of determining its dynamic state with respect to a target object is a key technology for performing spaceborne autonomous proximity operations. This core component is crucial in developing robust and reliable Guidance, Navigation and Control techniques in the field of spacecraft formation flight, on-orbit servicing, rendezvous and docking and active debris removal. This paper describes the development of a relative navigation strategy relying on the sole information provided by a stereoscopic vision system. The performances of the estimation approach are assessed by means of both orbital numerical simulations and experimental tests on the ground. The experimental activities are conducted in a representative dynamic environment within the context of the SPARTANS ground-based spacecraft simulator facility under development at the University of Padova.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"45 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114667119","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
UAV Intelligent Chemical Multisensor Payload for Networked and Impromptu Gas Monitoring Tasks 用于网络化和即兴气体监测任务的无人机智能化学多传感器载荷
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453543
M. Carrozzo, S. De Vito, E. Esposito, M. Salvato, F. Formisano, E. Massera, G. Di Francia, P. D. Veneri, M. Iadaresta, A. Mennella
{"title":"UAV Intelligent Chemical Multisensor Payload for Networked and Impromptu Gas Monitoring Tasks","authors":"M. Carrozzo, S. De Vito, E. Esposito, M. Salvato, F. Formisano, E. Massera, G. Di Francia, P. D. Veneri, M. Iadaresta, A. Mennella","doi":"10.1109/METROAEROSPACE.2018.8453543","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453543","url":null,"abstract":"This electronic Air quality is nowadays a primary concern in several cities. More generally pollutant and toxic gases continuously, incidentally or purposedly released are now considered to be extremely relevant for their severe adverse health effects to exposed citizens. In this view, low cost smart chemical multisensors are arising as a reliable source for indicative data on Air Quality. Low cost UAVs are versatile platforms capable to host playloads integrating multi sensor technologies for short term, mobile monitoring tasks. The recently proposed tethered UAV platforms can be deemed as interesting solutions to build and rapidly deploy impromptu networks of air quality analyzers for short-term and focused environmental monitoring actions. In this work, we propose the integration of the ENEA MONICA multisensor platform as a measurement payload for the TopView SAV-ES UAV. The prototype has been flown on board of the SAV-ES platform for a test flight targeting the measurement of a plume generated with a brushwood controlled fire. The functional proof of concept flight have confirmed the possibility to use MONICA as a measurement payload for the targeted platform.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"39 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130677764","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 8
Synthesis of Amorphous Mg-Carbonates for the Application in the Production of Advanced Materials 无定形碳酸镁的合成及其在先进材料生产中的应用
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453526
C. De Vito, L. Medeghini, S. Mignardi, F. Leccese
{"title":"Synthesis of Amorphous Mg-Carbonates for the Application in the Production of Advanced Materials","authors":"C. De Vito, L. Medeghini, S. Mignardi, F. Leccese","doi":"10.1109/METROAEROSPACE.2018.8453526","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453526","url":null,"abstract":"Carbonation experiments were performed to investigate the appropriateness of hydrate-amorphous carbonate minerals as well as their transformation products as sink of anthropogenic carbon dioxide. After the direct synthesis of these Mg-carbonates, in order to investigate the morphology of these amorphous materials SEM and XRPD have been used. These products can usefully involved producing advanced materials for industrial application.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"32 6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125733311","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Study on Vacuum Leak Calibration Technology Based on Static Cumulative Comparison Method 基于静态累积比较法的真空泄漏标定技术研究
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453564
Z. Lan, Cheng Yong-jun, Sun Wen-Jun, C. Lian, Li Ya-Li, Feng Tian-you
{"title":"Study on Vacuum Leak Calibration Technology Based on Static Cumulative Comparison Method","authors":"Z. Lan, Cheng Yong-jun, Sun Wen-Jun, C. Lian, Li Ya-Li, Feng Tian-you","doi":"10.1109/METROAEROSPACE.2018.8453564","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453564","url":null,"abstract":"In order to solve the problem of accurate calibration of vacuum leaks with very small leak rate (less than 10−10 Pam3 / s), a calibration method based on the static cumulative comparison method is proposed. The method mainly uses a quadrupole mass spectrometer to compare ion current rise rates from standard gas flow meter and vacuum leak during static accumulation, and then the calibration on vacuum leak is achieved. In this paper, the calibration method based on static cumulative comparison is introduced, which includes apparatus principle, calibration process, calibration result processing and so on, and the factors of reducing the measurement uncertainty of calibration result are put forward.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"247 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134179034","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Design of a Microwave Sensor for Fuel Quality Monitoring 一种用于燃油质量监测的微波传感器设计
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453606
G. Andria, F. Attivissimo, A. Di Nisio, G. M. D'Aucelli, S. Camporeale, P. Pappalardi
{"title":"Design of a Microwave Sensor for Fuel Quality Monitoring","authors":"G. Andria, F. Attivissimo, A. Di Nisio, G. M. D'Aucelli, S. Camporeale, P. Pappalardi","doi":"10.1109/METROAEROSPACE.2018.8453606","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453606","url":null,"abstract":"The fuel of endothermic engines supplies chemical energy to be transformed into mechanical energy, lubricates precision parts in the components of the fuel system and cools metal surfaces that operate under friction conditions. The characteristics of the fuel must meet these three conditions so that the engine operates reliably. Water is the worst contaminant that affect engine operation. Therefore, fuel control is part of maintenance operations to extend the life of the engine, optimizing performance, preventing breakdowns and reducing fuel consumption and harmful atmospheric emissions. This paper reports the preliminary design of a sensor for real time monitoring of the fuel, integrated in the fuel system. The sensor must be low cost and able to detect anomalies in the fuel and deviations from normal operating conditions with good accuracy. Furthermore, given the aggressive nature of the fuel, the detection must be contactless. In particular, due to the different chemical nature of the fuel based on the geographical area of origin, it was decided to design sensors having detectivity that can be selected in a wide dynamic range. The chosen technology is based on microwave measurements.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129847678","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A Passive Cloud Detection System for UAV: Analysis of Issues, Impacts and Solutions 无人机被动云探测系统:问题、影响及解决方案分析
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453614
F. Funk, P. Stütz
{"title":"A Passive Cloud Detection System for UAV: Analysis of Issues, Impacts and Solutions","authors":"F. Funk, P. Stütz","doi":"10.1109/METROAEROSPACE.2018.8453614","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453614","url":null,"abstract":"Lightweight unmanned aerial vehicles (UAVs) are highly susceptible to the presence of clouds. In contrast to other UAVs or airplanes, clouds directly pose a danger to their structural health. Furthermore, clouds indicate other weather phenomena appearing in their vicinity, such as turbulences or icing. Additionally, the stringent platform limitations of lightweight UAVs, for example, mass and energy consumption do not allow the use of the classic on-board weather sensor, the weather radar. Therefore, a passive cloud detection system for on-board use, based on an imaging sensor, was proposed and developed. The focus of this paper lies on the challenges of the used measurement methods. An analysis of each step identifies the issues during cloud detection and mapping. Calculations and tests in virtual and real environments show their impacts. Eventually, solutions or mitigations are presented respectively.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"58 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129966784","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 3
High Update Rate Star Tracker for Gyroless Spacecraft Operation 用于无陀螺航天器运行的高更新率星跟踪器
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453507
Mikael Marin, H. Bang
{"title":"High Update Rate Star Tracker for Gyroless Spacecraft Operation","authors":"Mikael Marin, H. Bang","doi":"10.1109/METROAEROSPACE.2018.8453507","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453507","url":null,"abstract":"Traditional star trackers are designed for high accuracy but low update rate and rely on rate gyros to interpolate between measurements. However, the available rate gyros are either noisy, or expensive and heavy. The proposed work demonstrates the advantage of sacrificing some of the star tracker's accuracy for a higher update rate. As a result, aside from removing the need for a rate gyro, Attitude Determination and Control Systems overall performances are increased. The proposed star tracker achieved a 0.001 ° accurate Attitude Determination, with a 98.8% sky coverage at a 50Hz update rate. In addition, the image processing and star matching algorithm are designed to be efficiently implemented as a fully pipelined single-pass FPGA circuit.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"87 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132182823","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Embedded Wheel Force Sensor for Aircraft Landing Gear Testing 用于飞机起落架测试的嵌入式轮力传感器
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453511
J. Pytka, J. Józwik, T. Łyszczyk, E. Gnapowski
{"title":"Embedded Wheel Force Sensor for Aircraft Landing Gear Testing","authors":"J. Pytka, J. Józwik, T. Łyszczyk, E. Gnapowski","doi":"10.1109/METROAEROSPACE.2018.8453511","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453511","url":null,"abstract":"The paper presents a wheel dynamometer system developed for testing aircraft landing gear. The purpose of the dynamometer is to measure forces and moments acting on an aircraft landing gear wheel. The dynamometer was designed with the use of strain gages, as an autonomous measuring device, with a wireless data transferring system. The presented system was designed for the PZL 104 Wilga 35A multipurpose aircraft, but it could be re-designed for any other general aviation, light aircraft. The paper contains detailed descriptions of the design and development as well as sample results from early test measurements. Certification for ground and flight tests of airplanes has been considered for the presented dynamometer system.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"55 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130771021","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 7
Dielectric Characterization of Ice/Na2SO4·10H2O Mixtures: Implications for Radar Investigations of Icy Satellites 冰/Na2SO4·10H2O混合物的介电特性:对冰冻卫星雷达探测的启示
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453549
B. Cosciotti, E. Mattei, E. Pettinelli, Francesco Gabbai, F. Di Paolo, S. Lauro
{"title":"Dielectric Characterization of Ice/Na2SO4·10H2O Mixtures: Implications for Radar Investigations of Icy Satellites","authors":"B. Cosciotti, E. Mattei, E. Pettinelli, Francesco Gabbai, F. Di Paolo, S. Lauro","doi":"10.1109/METROAEROSPACE.2018.8453549","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453549","url":null,"abstract":"Jupiter satellites will be the object of study of future ESA and NASA missions: JUICE and Europa. In particular these missions have been motivated to understand the geological activity from the subsurface to the surface and also to constrain the minimal thickness of the ice shell. In fact, both missions will host a radar on board: JUICE will investigate the subsurface through RIME, an ice penetrating radar sounder operating on a single frequency band, centered at 9 MHz, that should be able to penetrate up to 9 km (depending on the crust properties) below the frozen surface, with a vertical resolution of up to 30 meters in the ice, while REASON is a dual frequency radar (9 and 60 MHz) that will be hosted on Europa mission. The performance of both radars depends on the dielectric behavior of the icy crusts, which in turn are related to the temperature and chemical constituents of the icy shells. In this context, we have performed a series of dielectric measurements as a function of frequency on different sodium sulfate decahydrate mixtures cooled down to typical temperatures of Jovian satellites. Our objective is to evaluate the effective penetration capability of low-frequency sounder radars in detecting subsurface structures characterized by variations in the electrical properties of the ice. The results of this experimental activity revealed that these salty ice analogs showed a decrease in attenuation with the temperature drop, increasing the radar signal possibilities to penetrate inside the satellite","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"30 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124918739","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
MET4F: A Tool for Providing in Near Real-Time Weather Information on Board MET4F:提供船上近实时天气信息的工具
2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453547
M. Montesarchio, A. Zollo, P. Mercogliano
{"title":"MET4F: A Tool for Providing in Near Real-Time Weather Information on Board","authors":"M. Montesarchio, A. Zollo, P. Mercogliano","doi":"10.1109/METROAEROSPACE.2018.8453547","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453547","url":null,"abstract":"In order to increase the weather awareness on board, at CIRA (Italian Aerospace Research Center) it is under development a general system able to provide, in near-real time, forecast and monitored weather information along the flight route, gathering and integrating data from different sources. MET4F (METeorological data for FLARE) is a new tool, within this system, devoted to provide the over mentioned weather information through the dispatch of a binary message from an on ground control station to an Unmanned Air Vehicle (UAV). The message format follows the protocol adopted by the CIRA Remotely Piloted Aircraft System and allows an automatic flight reconfiguration, also on the basis of the weather information.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121987043","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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