Diagnosing low earth orbit satellite anomalies using NOAA-15 electron data associated with geomagnetic perturbations
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- 資料種別
- 記事
- 著者・編者
- Nizam AhmadDhani HerdiwijayaThomas Djamaluddin
- 出版年月日等
- 2018-05-29
- 出版年(W3CDTF)
- 2018-05-29
- タイトル(掲載誌)
- EPS : Earth, Planets and Space
- 巻号年月日等(掲載誌)
- 70(91)
- 掲載巻
- 70(91)
- ISSN(掲載誌)
- 1880-5981
- ISSN-L(掲載誌)
- 1343-8832
- 本文の言語コード
- eng
- DOI
- 10.1186/s40623-018-0852-2
- 国立国会図書館永続的識別子
- info:ndljp/pid/11125859
- コレクション(共通)
- コレクション(障害者向け資料:レベル1)
- コレクション(個別)
- 国立国会図書館デジタルコレクション > 電子書籍・電子雑誌 > その他
- 収集根拠
- オンライン資料収集制度
- 受理日(W3CDTF)
- 2018-08-10T20:26:03+09:00
- 保存日(W3CDTF)
- 2018-08-10
- 記録形式(IMT)
- application/pdf
- オンライン閲覧公開範囲
- 国立国会図書館内限定公開
- デジタル化資料送信
- 図書館・個人送信対象外
- 遠隔複写可否(NDL)
- 可
- 掲載誌(国立国会図書館永続的識別子)
- info:ndljp/pid/11067456
- 連携機関・データベース
- 国立国会図書館 : 国立国会図書館デジタルコレクション
- 要約等
- A satellite placed in space is constantly affected by the space environment, resulting in various impacts from temporary faults to permanent failures depending on factors such as satellite orbit, solar and geomagnetic activities, satellite local time, and satellite construction material. Anomaly events commonly occur during periods of high geomagnetic activity that also trigger plasma variation in the low Earth orbit (LEO) environment. In this study, we diagnosed anomalies in LEO satellites using electron data from the Medium Energy Proton and Electron Detector onboard the National Oceanic and Atmospheric Administration (NOAA)-15 satellite. In addition, we analyzed the fluctuation of electron flux in association with geomagnetic disturbances 3 days before and after the anomaly day. We selected 20 LEO anomaly cases registered in the Satellite News Digest database for the years 2000–2008. Satellite local time, an important parameter for anomaly diagnosis, was determined using propagated two-line element data in the SGP4 simplified general perturbation model to calculate the longitude of the ascending node of the satellite through the position and velocity vectors. The results showed that the majority of LEO satellite anomalies are linked to low-energy electron fluxes of 30–100 keV and magnetic perturbations that had a higher correlation coefficient (~ 90%) on the day of the anomaly. The mean local time calculation for the anomaly day with respect to the nighttime migration of energetic electrons revealed that the majority of anomalies (65%) occurred on the night side of Earth during the dusk-to-dawn sector of magnetic local time.
- DOI
- 10.1186/s40623-018-0852-2
- オンライン閲覧公開範囲
- インターネット公開
- 著作権情報
- © The Author(s) 2018.This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
- 関連情報(URI)
- 参照
- The Particle-In-Cell simulation on LEO spacecraft charging and the wake structure using EMSES
- 参照
- Identification of substorms within stormsSpace environment effects and satellite designCorrelation of GEO Comsat Anomalies and Space Weather Phenomena for Improved Satellite Performance and Risk MitigationRevisiting Spacetrack Report #3Energetic electron flux behavior at low L-shells and its relation to the South Atlantic AnomalyPOES MEPED differential flux retrievals and electron channel contamination correctionMagnetic signatures for satellite anomaliesPhysics of the Earth’s Space EnvironmentUse of POES SEM‐2 observations to examine radiation belt dynamics and energetic electron precipitation into the atmosphereCharacteristics of spacecraft charging in low Earth orbitThe relation of high- and low-orbit satellite anomalies to different geophysical parametersSpacecraft-Environment InteractionsStatistical relationships between satellite anomalies at geostationary orbit and high-energy particlesSEAES‐GEO: A spacecraft environmental anomalies expert system for geosynchronous orbitSpacecraft operational anomalies and space weather impact hazardsSpacecraft charging anomaly on a low-altitude satellite in an auroraElectron flux enhancement in the inner radiation belt during moderate magnetic stormsStatistical properties of the surface‐charging environment at geosynchronous orbitCorrelation of GSO satellite anomalies with space weather dataThe long-term effects of space weather on satellite operationsAnalysis of environmentally induced spacecraft anomaliesAnalysis of GEO spacecraft anomalies: Space weather relationshipsWhat is a geomagnetic storm?A review of plasma interactions with spacecraft in low Earth orbitAuroral particle precipitation characterized by the substorm cycleHigh‐level spacecraft charging in the low‐altitude polar auroral environmentOrigin of energetic electron precipitation >30 keV into the atmosphereCorrecting the NOAA/MEPED energetic electron fluxes for detector efficiency and proton contamination
- 連携機関・データベース
- 国立情報学研究所 : CiNii Research
- 提供元機関・データベース
- 学術機関リポジトリデータベース雑誌記事索引データベースCrossrefCiNii Articles科学研究費助成事業データベース科学研究費助成事業データベースCrossref
- 書誌ID(NDLBibID)
- 11125859
- NII論文ID
- 120006477550
- 要約等
- P(論文)研究助成による研究報告Research Paper Regarding a Research or Project Conducted with a Grant from KUIS
- DOI
- 10.69236/0000000599
- 関連情報(URI)
- 連携機関・データベース
- 国立情報学研究所 : CiNii Research
- 提供元機関・データベース
- Japan Link Center学術機関リポジトリデータベース雑誌記事索引データベースCiNii Articles科学研究費助成事業データベース
- 書誌ID(NDLBibID)
- 11125859
- NII論文ID
- 110008154854