Diagnosing low earth orbit satellite anomalies using NOAA-15 electron data associated with geomagnetic perturbations
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DOI[10.1186/s40623-018-0852-2]to the data of the same series
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- Material Type
- 記事
- Author/Editor
- Nizam AhmadDhani HerdiwijayaThomas Djamaluddin
- Publication, Distribution, etc.
- Publication Date
- 2018-05-29
- Publication Date (W3CDTF)
- 2018-05-29
- Periodical title
- EPS : Earth, Planets and Space
- No. or year of volume/issue
- 70(91)
- Volume
- 70(91)
- ISSN (Periodical Title)
- 1880-5981
- ISSN-L (Periodical Title)
- 1343-8832
- Text Language Code
- eng
- DOI
- 10.1186/s40623-018-0852-2
- Persistent ID (NDL)
- info:ndljp/pid/11125859
- Collection
- Collection (Materials For Handicapped People:1)
- Collection (particular)
- 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
- Acquisition Basis
- オンライン資料収集制度
- Date Accepted (W3CDTF)
- 2018-08-10T20:26:03+09:00
- Date Captured (W3CDTF)
- 2018-08-10
- Format (IMT)
- application/pdf
- Access Restrictions
- 国立国会図書館内限定公開
- Service for the Digitized Contents Transmission Service
- 図書館・個人送信対象外
- Availability of remote photoduplication service
- 可
- Periodical Title (URI)
- Periodical Title (Persistent ID (NDL))
- info:ndljp/pid/11067456
- Data Provider (Database)
- 国立国会図書館 : 国立国会図書館デジタルコレクション
- Summary, etc.
- 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
- Access Restrictions
- インターネット公開
- Rights (production)
- © 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.
- Related Material (URI)
- Is Referenced By
- The Particle-In-Cell simulation on LEO spacecraft charging and the wake structure using EMSES
- References
- 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
- Data Provider (Database)
- 国立情報学研究所 : CiNii Research
- Original Data Provider (Database)
- 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
- Bibliographic ID (NDL)
- 11125859
- NAID
- 120006477550
- Summary, etc.
- 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
- Related Material (URI)
- Data Provider (Database)
- 国立情報学研究所 : CiNii Research
- Original Data Provider (Database)
- 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
- Bibliographic ID (NDL)
- 11125859
- NAID
- 110008154854