Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788968
E. Dunkin, T. Duggan, R. P. Noyce
The electromagnetic Radio Frequency environment which electro-explosive devices (EEDs) may experience in service and how this can affect the Hazards of Electromagnetic Radiation to Ordinance (HERO) safety are discussed. The uses for these types of devices in the aerospace industry are for both safety consequences and mission related systems. This paper discusses the different methods used for instrumenting EEDs in the past and presently, and the advantages and disadvantages of each type of instrumentation. Additionally, improvements that have been made in recent years are described, developing instrumentation techniques that are more reliable and repeatable with good sensitivities for each individual device and allow extrapolation of measurements. This paper also discusses the most common forms of instrumentation used today for testing in a High Intensity Radiated Field (HIRF) environment and where these methods were developed from.
{"title":"Hazards Of Electromagnetic Radiation to Ordnance (HERO) Instrumentation Developments for High Intensity Radiated Field (HIRF) Testing of Aircraft","authors":"E. Dunkin, T. Duggan, R. P. Noyce","doi":"10.23919/AeroEMC.2019.8788968","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788968","url":null,"abstract":"The electromagnetic Radio Frequency environment which electro-explosive devices (EEDs) may experience in service and how this can affect the Hazards of Electromagnetic Radiation to Ordinance (HERO) safety are discussed. The uses for these types of devices in the aerospace industry are for both safety consequences and mission related systems. This paper discusses the different methods used for instrumenting EEDs in the past and presently, and the advantages and disadvantages of each type of instrumentation. Additionally, improvements that have been made in recent years are described, developing instrumentation techniques that are more reliable and repeatable with good sensitivities for each individual device and allow extrapolation of measurements. This paper also discusses the most common forms of instrumentation used today for testing in a High Intensity Radiated Field (HIRF) environment and where these methods were developed from.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131529490","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788932
H. Kuegler, D. Lentz
A new test facility was designed and built in order to heat up the Solar Orbiter Heat-Shield to 560° Celsius in vacuum conditions. A heated plate of steal with the dimension of 3m x 2.4m was used as a heat source. This heated plate was heated by radiated heat flux of a heating system with seven heating circles consisted of nine heating coils running. The electric current was up to 300A RMS at a voltage up to 60V at the power grid frequency of 50Hz in vacuum conditions. In order to ensure the magnetic requirements of Solar Orbiter it was indicated that no piece of flight hardware shall be exposed to magnetic fields higher than $200 mumathrm{T}$. The decision was taken to monitor the process of development with respect to magnetic cleanliness. The overall magnetic design/modelling process is presented as well as the verification steps performed on the real 600°C Hot Plate Setup.
为了在真空条件下将太阳轨道隔热板加热到560摄氏度，设计并建造了一个新的测试设备。热源采用尺寸为3m x 2.4m的加热钢板。该加热板由一个由九个加热盘管组成的七个加热循环的加热系统的辐射热流加热。在真空条件下，电网频率50Hz，电压60V，电流RMS可达300A。为了保证太阳轨道飞行器的磁场要求，指出任何飞行硬件都不能暴露在高于200美元的磁场中。决定监测磁洁净度的发展过程。介绍了整体磁性设计/建模过程以及在实际600°C热板设置上执行的验证步骤。
{"title":"Determination of Magnetic Effect of the 600°C Hot Plate Setup for Testing the Heat Shield of Solar-Orbiter","authors":"H. Kuegler, D. Lentz","doi":"10.23919/AeroEMC.2019.8788932","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788932","url":null,"abstract":"A new test facility was designed and built in order to heat up the Solar Orbiter Heat-Shield to 560° Celsius in vacuum conditions. A heated plate of steal with the dimension of 3m x 2.4m was used as a heat source. This heated plate was heated by radiated heat flux of a heating system with seven heating circles consisted of nine heating coils running. The electric current was up to 300A RMS at a voltage up to 60V at the power grid frequency of 50Hz in vacuum conditions. In order to ensure the magnetic requirements of Solar Orbiter it was indicated that no piece of flight hardware shall be exposed to magnetic fields higher than $200 mumathrm{T}$. The decision was taken to monitor the process of development with respect to magnetic cleanliness. The overall magnetic design/modelling process is presented as well as the verification steps performed on the real 600°C Hot Plate Setup.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"19 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134551789","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788927
A. T. Baklezos, C. D. Nikolopoulos, S. Spantideas, E. G. Chatzineofytou, M. Nicoletto, I. Marziali, D. Boschetti, Christos N. Capsalis
In this work, the test procedures and modeling results of low frequency (LF) electric and magnetic fields radiated by spacecraft equipment are implemented on near field measurements of the Command & Data Handling Management Unit (CDMU) of GOCE space mission. Specifically, the unit's LF electromagnetic signature is acquired up to 200 kHz and the frequencies that exhibit emissions are identified for both electric and magnetic field contributions. The measurements and modeling procedure are performed targeting to capture and characterize the steady state operation of the CDMU. The modeling methods presented in this work rely on measurements conducted in the frame of ESA's study on Pre-Verification of THOR Electro-Magnetic Cleanliness Approach.
{"title":"Steady State Emissions Modeling of Low Frequency Magnetic and Electric Fields Generated by GOCE CDMU","authors":"A. T. Baklezos, C. D. Nikolopoulos, S. Spantideas, E. G. Chatzineofytou, M. Nicoletto, I. Marziali, D. Boschetti, Christos N. Capsalis","doi":"10.23919/AeroEMC.2019.8788927","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788927","url":null,"abstract":"In this work, the test procedures and modeling results of low frequency (LF) electric and magnetic fields radiated by spacecraft equipment are implemented on near field measurements of the Command & Data Handling Management Unit (CDMU) of GOCE space mission. Specifically, the unit's LF electromagnetic signature is acquired up to 200 kHz and the frequencies that exhibit emissions are identified for both electric and magnetic field contributions. The measurements and modeling procedure are performed targeting to capture and characterize the steady state operation of the CDMU. The modeling methods presented in this work rely on measurements conducted in the frame of ESA's study on Pre-Verification of THOR Electro-Magnetic Cleanliness Approach.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"17 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134251620","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788935
G. Erdős, L. Hevesi, I. Lemperger, J. Nagy, Z. Németh, V. Wesztergom
Electromagnetically clean room is planned to be built in the Széchenyi István Geophysical Observatory in western Hungary. The environmental magnetic field will be reduced by five order of magnitude, which is well below the interplanetary magnetic field near the Earth. One of the application of the laboratory is to support magnetic cleanliness program for space equipments. Moreover, in particular for space applications, it is planned to develop, test and calibrate a new generation of magnetometers called SERF (Spin Exchange Relaxation-Free). Active compensation of the terrestrial field will be achieved by means of large coils with current determined from the actual field, which is measured through a magnetometer placed in the observatory. Passive shielding will be provided by a cube shaped room covered with two layers of mumetal. The novelty of the facility is that the two shielding techniques will be harmonized. To this purpose, detailed model calculations were performed in order to determine the best setup for the coils. The results of the numerical calculations show that the size of the compensating coils should be much larger than the size of the room covered with mumetal layers.
{"title":"Installation of an Electromagnetic Test Facility in Hungary","authors":"G. Erdős, L. Hevesi, I. Lemperger, J. Nagy, Z. Németh, V. Wesztergom","doi":"10.23919/AeroEMC.2019.8788935","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788935","url":null,"abstract":"Electromagnetically clean room is planned to be built in the Széchenyi István Geophysical Observatory in western Hungary. The environmental magnetic field will be reduced by five order of magnitude, which is well below the interplanetary magnetic field near the Earth. One of the application of the laboratory is to support magnetic cleanliness program for space equipments. Moreover, in particular for space applications, it is planned to develop, test and calibrate a new generation of magnetometers called SERF (Spin Exchange Relaxation-Free). Active compensation of the terrestrial field will be achieved by means of large coils with current determined from the actual field, which is measured through a magnetometer placed in the observatory. Passive shielding will be provided by a cube shaped room covered with two layers of mumetal. The novelty of the facility is that the two shielding techniques will be harmonized. To this purpose, detailed model calculations were performed in order to determine the best setup for the coils. The results of the numerical calculations show that the size of the compensating coils should be much larger than the size of the room covered with mumetal layers.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"21 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114526535","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788928
J. Kasper, M. Magdowski, R. Vick, L. Galeev, Genadii Iukhtanov, Evgenii Fedorov, A. Ferenets
The coupling of plane waves with a specific time function, incident direction and polarization to a transmission line network (TLN) consisting of three single-wire transmission lines is investigated. The network is analyzed simulatively and experimentally in a GTEM cell. The coupled voltage to the TLN is investigated in frequency domain and in time domain. The investigation in time domain allows taking into account non-linear loads like diodes. The simulations were done in LTspice, a simulation tool for circuit simulation. The model is validated against an existing frequency domain solution for linear loads. Furthermore, both of the simulated results are compared to measured ones.
{"title":"Time Domain Investigation of the Plane Wave Coupling to a Non-Lineary Loaded Transmission Line Network","authors":"J. Kasper, M. Magdowski, R. Vick, L. Galeev, Genadii Iukhtanov, Evgenii Fedorov, A. Ferenets","doi":"10.23919/AeroEMC.2019.8788928","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788928","url":null,"abstract":"The coupling of plane waves with a specific time function, incident direction and polarization to a transmission line network (TLN) consisting of three single-wire transmission lines is investigated. The network is analyzed simulatively and experimentally in a GTEM cell. The coupled voltage to the TLN is investigated in frequency domain and in time domain. The investigation in time domain allows taking into account non-linear loads like diodes. The simulations were done in LTspice, a simulation tool for circuit simulation. The model is validated against an existing frequency domain solution for linear loads. Furthermore, both of the simulated results are compared to measured ones.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"149 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114443794","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788955
S. Leman, R. Omarouayache, F. Hoëppe, A. Piche
This paper presents the post-processing methodology devoted to the Near-Field-Scanning (NFS) to provide assistance in ElectroMagnetic Compatibility (EMC) design phases of complex electronics products. A major challenge for spacecraft manufacturers for incoming year concerns the control of units Radiated Emissions (RE). Indeed, high speed links could induce RE non-compliance for units in on-board receiver frequencies (ex: GPS, TCR…). To avoid additional test campaign or system level analyses, Near Field techniques could be a powerful way to anticipate RE non-conformities in unit design phase. Based both on NFS (only $H_{x}$ and $H_{y}$ magnetic components very closed to the Printed Circuit Board (PCB)), and on Shielding enclosure Effectiveness (SE) characterization, the proposed “NFS2RE” (Near Field Scanning to Radiated Emission Test) methodology allows: 1)RE-Test prediction of PCB in free space condition from only $H_{x}$ and $H_{y}$ NFS 2)Prediction of Shielding PCB's enclosure attenuation on RE-Test from SE characterization
{"title":"Prediction of Electronic Unit Radiated Emissions from Both PCB Near Field and Shielding Enclosure Characterization","authors":"S. Leman, R. Omarouayache, F. Hoëppe, A. Piche","doi":"10.23919/AeroEMC.2019.8788955","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788955","url":null,"abstract":"This paper presents the post-processing methodology devoted to the Near-Field-Scanning (NFS) to provide assistance in ElectroMagnetic Compatibility (EMC) design phases of complex electronics products. A major challenge for spacecraft manufacturers for incoming year concerns the control of units Radiated Emissions (RE). Indeed, high speed links could induce RE non-compliance for units in on-board receiver frequencies (ex: GPS, TCR…). To avoid additional test campaign or system level analyses, Near Field techniques could be a powerful way to anticipate RE non-conformities in unit design phase. Based both on NFS (only $H_{x}$ and $H_{y}$ magnetic components very closed to the Printed Circuit Board (PCB)), and on Shielding enclosure Effectiveness (SE) characterization, the proposed “NFS2RE” (Near Field Scanning to Radiated Emission Test) methodology allows: 1)RE-Test prediction of PCB in free space condition from only $H_{x}$ and $H_{y}$ NFS 2)Prediction of Shielding PCB's enclosure attenuation on RE-Test from SE characterization","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"37 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131627759","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788961
Tonus Serge, Rispal Mathieu
This paper is about the Shielding Effectiveness (SE) measurement realized by THALES ALENIA SPACE in Toulouse on the microwave passive units and devices implemented into the communication module of the satellite payloads. In order to verify EMC design rules efficiency and the associated workmanship, these SE measurements are mandatory by the prime on all the microwave Flying Model units. Moreover, these SE measurements are also used to quantify the efficiency of the EMC design protections (Shielding gaskets or materials, interface connectors….) implemented on the RF (Radio Frequency) units during conception phase. These SE tests are performed using an oversized cavity called Mode Stirred Reverberation Chamber (MSRC) since 2007. Typical tests results and associated methodology are presented in this paper.
{"title":"Shielding Effectiveness Measurements on Satellite Microwave Passive Elements Using Reverberation Chamber Test Method","authors":"Tonus Serge, Rispal Mathieu","doi":"10.23919/AeroEMC.2019.8788961","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788961","url":null,"abstract":"This paper is about the Shielding Effectiveness (SE) measurement realized by THALES ALENIA SPACE in Toulouse on the microwave passive units and devices implemented into the communication module of the satellite payloads. In order to verify EMC design rules efficiency and the associated workmanship, these SE measurements are mandatory by the prime on all the microwave Flying Model units. Moreover, these SE measurements are also used to quantify the efficiency of the EMC design protections (Shielding gaskets or materials, interface connectors….) implemented on the RF (Radio Frequency) units during conception phase. These SE tests are performed using an oversized cavity called Mode Stirred Reverberation Chamber (MSRC) since 2007. Typical tests results and associated methodology are presented in this paper.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127469997","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788953
J. A. Puértolas, R. Perraud
This paper presents a study on the electromagnetic crosstalk characteristics of planar superposed cabling structures. A particular technological development targeting external Launcher electrical raceways and called Electro-Structural Composite is presented and analysed. The final objective for system integrators is to build up and master electrical segregation rules to assure the conducted electromagnetic compatibility of the links connecting different electric/electronic equipment placed on the spacecraft (i.e. power, signal, bus, status, electro-pyrotechnical…).
{"title":"Conducted Coupling Analysis of Flat Cabling Structures for Launcher Applications: Electrostructural Composite","authors":"J. A. Puértolas, R. Perraud","doi":"10.23919/AeroEMC.2019.8788953","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788953","url":null,"abstract":"This paper presents a study on the electromagnetic crosstalk characteristics of planar superposed cabling structures. A particular technological development targeting external Launcher electrical raceways and called Electro-Structural Composite is presented and analysed. The final objective for system integrators is to build up and master electrical segregation rules to assure the conducted electromagnetic compatibility of the links connecting different electric/electronic equipment placed on the spacecraft (i.e. power, signal, bus, status, electro-pyrotechnical…).","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"17 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127835366","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788921
G. Spadacini, F. Grassi, S. Pignari, P. Bisognin, A. Piche
Some promising test procedures were recently developed as alternative approaches to radiated susceptibility (RS) verifications for unit-level test setups, with specific (but non-exclusive) reference to aerospace equipment. All test methods are based on the injection of conducted disturbances in the cable under test via suitable coupling devices and fall into two categories: a deterministic and a statistical equivalence scheme. While the former aims at the exact reproduction of RS effects, the latter enforces correlation of outcomes in statistical terms. In this paper, these different approaches are reviewed and critically discussed by the light of merit criteria including cost saving, training, intrusiveness, time consumption, complexity, repeatability and reproducibility, limitations of the equivalence.
{"title":"Alternative Approaches to Radiated Susceptibility Testing at Unit Level: Trade-Off Analysis of Proposed Solutions","authors":"G. Spadacini, F. Grassi, S. Pignari, P. Bisognin, A. Piche","doi":"10.23919/AeroEMC.2019.8788921","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788921","url":null,"abstract":"Some promising test procedures were recently developed as alternative approaches to radiated susceptibility (RS) verifications for unit-level test setups, with specific (but non-exclusive) reference to aerospace equipment. All test methods are based on the injection of conducted disturbances in the cable under test via suitable coupling devices and fall into two categories: a deterministic and a statistical equivalence scheme. While the former aims at the exact reproduction of RS effects, the latter enforces correlation of outcomes in statistical terms. In this paper, these different approaches are reviewed and critically discussed by the light of merit criteria including cost saving, training, intrusiveness, time consumption, complexity, repeatability and reproducibility, limitations of the equivalence.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126909874","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}
Pub Date : 2019-05-01DOI: 10.23919/AeroEMC.2019.8788945
F. Treviso, R. Trinchero, F. Canavero
This paper focuses on the development and the experimental validation of a physical-based model for the SpaceWire (SpW) cable (Variant 01) terminated by two micro D-type connectors. The model for the SpW cable relies on the frequency-dependent per-unit-length parameters computed from the available information of its cross-section and materials via a 2D simulation. On the other hand, the D-type connector model is obtained from the simulation results provided by its 3D representation in CST MICROWAVE STUDIO. The two models are then combined together and implemented in HSPICE by means of their circuit equivalents. The accuracy of the proposed models is then experimentally validated by considering the scattering parameters measured via an ad-hoc measurement setup.
{"title":"Validation of a Physical-Based Model for a Spacewire Cable","authors":"F. Treviso, R. Trinchero, F. Canavero","doi":"10.23919/AeroEMC.2019.8788945","DOIUrl":"https://doi.org/10.23919/AeroEMC.2019.8788945","url":null,"abstract":"This paper focuses on the development and the experimental validation of a physical-based model for the SpaceWire (SpW) cable (Variant 01) terminated by two micro D-type connectors. The model for the SpW cable relies on the frequency-dependent per-unit-length parameters computed from the available information of its cross-section and materials via a 2D simulation. On the other hand, the D-type connector model is obtained from the simulation results provided by its 3D representation in CST MICROWAVE STUDIO. The two models are then combined together and implemented in HSPICE by means of their circuit equivalents. The accuracy of the proposed models is then experimentally validated by considering the scattering parameters measured via an ad-hoc measurement setup.","PeriodicalId":436679,"journal":{"name":"2019 ESA Workshop on Aerospace EMC (Aerospace EMC)","volume":"142 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129514896","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}
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