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

Methods for Testing Military Radars Produced in Poland 波兰生产的军用雷达测试方法

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453542

Mariusz Pakowski, M. Brzozowski, M. Michalczewski, Mirosław Myszka

引用次数: 7

Metrology Problems of WIG-Craft Motion Control wigg - craft运动控制的计量问题

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453590

A. Nebylov, Vladimir Nebylov, A. Knyazhsky

引用次数: 5

Upstream Wind Sensing for Small Unmanned Aerial Vehicles 小型无人机上游风感测

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453537

Simon C Watkins, Mohamed Abdulghani, S. Prudden, David Tennent, M. Marino, A. Fisher

引用次数: 0

Nickel Supported on Y2O3-ZrO2as Highly Selective and Stable CO2Methanation Catalyst for in-Situ Propellant Production on Mars y2o3 - zro2负载镍作为高选择性稳定的火星原位推进剂co2甲烷化催化剂

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453548

S. Tuti, I. Luisetto, F. Leccese, Jagadesh Kopula Kesavan, S. Casciardi

引用次数: 4

Measurements Optimization for Control of Distributed Parameter Systems 分布参数系统控制的测量优化

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453577

S. Brodsky, A. Nebylov, A. Panferov

引用次数: 0

Smart Air-Data Probe for Fault-Tolerant Flow Measurements 用于容错流量测量的智能空气数据探头

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453555

F. Schettini, G. Di Rito, R. Galatolo

{"title":"Smart Air-Data Probe for Fault-Tolerant Flow Measurements","authors":"F. Schettini, G. Di Rito, R. Galatolo","doi":"10.1109/METROAEROSPACE.2018.8453555","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453555","url":null,"abstract":"This paper deals with the development of a smart multi-hole probe for aircraft air data parameters. The system aims at the calculation of static and total pressures, and the angle-of-attack and angle-of-sideslip (fine output data) starting from the elaboration of the pressure measurements on holes (raw input data). The probe, characterized by fault-tolerant capabilities with respect the loss of one pressure data, is developed as an embedded system that includes MEMS pressure/temperature sensors and a control electronics implementing multiple reconstructions of the flow measurements, up to obtain fault-tolerant output data. The basic idea for the reconstruction algorithm is that, in the normal envelope of aircraft flow angles (≤15° for both attack and sideslip), the shape of the pressure field around the stagnation point of a hemispherical body is essentially independent from the flow angles. Thus, once characterised the aerodynamic flow at the aircraft installation for zero angle of attack and sideslip, the reconstruction is performed by minimising the errors between the five pressure measurements on the probe tip and the predictions of models imposing a set of locations of the stagnation point. The external geometry of the probe is designed and validated by CFD simulations. In particular, CFD simulations have been performed to verify both the basic concept and the capability of the algorithm to provide the flow angles even if one of the pressure measurements is not available. The work describes the reconstruction algorithm and the system development, from the conceptual phase, up to the manufacturing of the first prototype to be used for the experimental tests.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"72 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":"114090643","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

Testing an Electronic Nose for Pre-Bond NDT in Realistic CFRP Parts Assembly and Repair 电子鼻在实际碳纤维复合材料零件装配和维修中的粘结前无损检测测试

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453609

S. De Vito, M. Salvato, E. Massera, F. Formisano, M. Miglietta, E. Esposito, G. Di Francia

引用次数: 1

Dependable MPSoC-Based Mixed-Criticality Systems for Space Applications 空间应用中基于mpsoc的可靠混合临界系统

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453618

Stefano Esposito, M. Violante

{"title":"Dependable MPSoC-Based Mixed-Criticality Systems for Space Applications","authors":"Stefano Esposito, M. Violante","doi":"10.1109/METROAEROSPACE.2018.8453618","DOIUrl":"https://doi.org/10.1109/METROAEROSPACE.2018.8453618","url":null,"abstract":"Space applications' requirements, especially when scientific payload is considered, are rapidly increasing. A way to satisfy such requirements without increasing too much space, weight, and power consumption of the on-board equipment, is to exploit capabilities of new multi-processor system-on-chips (MPSoCs). A MPSoC-based computer would allow integration on a single equipment of several applications. However, there is not any space-qualified MPSoC, yet. This paper describes a mixed-criticality system (MCS) implementing a prototypical scientific payload computer for a space mission. The main focus is on the issue of using commercial-off-the-shelf (COTS) MPSoC in radioactive environment to deploy MCS implementing a payload computer. The paper states the beforementioned issue and a set of countermeasures to detect issues. The system is evaluated for dependability against single event effects (SEEs) through fault-injection simulation experiments. Results of such experiments are used to compute availability figures of a payload computer implementing described countermeasures, considering the radiation environment of the geostationary orbit.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"23 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":"125196932","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

Alignment Verification of a Star Tracker Cluster and a Space Telescope for Land-survey Satellite 陆地测量卫星星跟踪器星团与空间望远镜对准验证

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453562

Y. Somov, S. Butyrin, S. Somov, T. Somova

引用次数: 2

On the use of ExoMars Radar Doppler Altimeter for Descent Module Attitude Reconstruction ExoMars雷达多普勒高度计在下降舱姿态重建中的应用研究

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI: 10.1109/METROAEROSPACE.2018.8453569

M. Iorio, P. Pepe, Michela Veredice

引用次数: 0