Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Grigorios I. Koutantos"'
Autor:
Grigorios I. Koutantos, Christos D. Nikolopoulos, Christos N. Capsalis, Anargyros T. Baklezos
Publikováno v:
IEEE Transactions on Electromagnetic Compatibility. 62:1686-1692
A constant electromagnetic compatibility issue in the majority of space missions is the accurate EMI source identification and modeling. This is necessary in order to provide electromagnetic (EM) cleanliness in a specific area inside or outside the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5eabc7a0891786f5d75bfcb1a32b496a
https://doi.org/10.1109/temc.2019.2937379
https://doi.org/10.1109/temc.2019.2937379
Publikováno v:
2022 International Conference for Advancement in Technology (ICONAT).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f80d893d7aa628a3d6c32b8b993c9a78
https://doi.org/10.1109/iconat53423.2022.9725879
https://doi.org/10.1109/iconat53423.2022.9725879
Autor:
Anargyros T. Baklezos, Christos D. Nikolopoulos, Grigorios I. Koutantos, Christos N. Capsalis
Publikováno v:
IEEE Transactions on Electromagnetic Compatibility. 59:1457-1464
The majority of the space missions carry measuring instruments that are sensitive to electric fields and require stringent electromagnetic cleanliness. Therefore, the time variations of electric fields produced from spacecraft equipment have to be ch
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6ee7eaf9020b6535a3cc5008ac48a09
https://doi.org/10.1109/temc.2017.2685199
https://doi.org/10.1109/temc.2017.2685199
Autor:
Elpida G. Chatzineofytou, M. Nicoletto, Christos D. Nikolopoulos, Stylianos Tsatalas, Grigorios I. Koutantos, Anargyros T. Baklezos, I. Marziali, A. Junge, Klaus Mehlem, Christos N. Capsalis, D. Boschetti, Sotirios T. Spantideas
Publikováno v:
2019 ESA Workshop on Aerospace EMC (Aerospace EMC).
In this paper, an assessment of the measurement test results of the extremely low frequency (ELF) electromagnetic (EM) behaviour of several spacecraft units is demonstrated. The present work has been carried out in the framework of ESA's study Pre-Ve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::50fc21efc25b21bea50f74e1522dc124
https://doi.org/10.23919/aeroemc.2019.8788958
https://doi.org/10.23919/aeroemc.2019.8788958