Curriculum Vitaes
Profile Information
- Affiliation
- Assistant Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- 修士(理学)(東京大学)博士(理学)(東京大学)
- J-GLOBAL ID
- 201901006861784502
- researchmap Member ID
- B000359529
Research Areas
1Research History
5-
Sep, 2007 - Mar, 2010
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Apr, 2007 - Aug, 2007
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Apr, 2006 - Mar, 2007
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Apr, 2003 - Mar, 2006
Education
3-
Apr, 2003 - Mar, 2006
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Apr, 2001 - Mar, 2003
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- Mar, 2001
Committee Memberships
1-
2008 - 2010
Papers
89-
Journal of Geophysical Research: Space Physics, Jul, 2025
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Geophysical Research Letters, May 16, 2025
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Journal of Geophysical Research: Space Physics, Dec, 2024
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Journal of Geophysical Research: Space Physics, Nov, 2024
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Journal of Geophysical Research: Space Physics, 129(11), Oct 28, 2024Abstract Near‐equatorial measurements of energetic electron fluxes, in combination with numerical simulation, are widely used for monitoring of the radiation belt dynamics. However, the long orbital periods of near‐equatorial spacecraft constrain the cadence of observations to once per several hours or greater, that is, much longer than the mesoscale injections and rapid local acceleration and losses of energetic electrons of interest. An alternative approach for radiation belt monitoring is to use measurements of low‐altitude spacecraft, which cover, once per hour or faster, the latitudinal range of the entire radiation belt within a few minutes. Such an approach requires, however, a procedure for mapping the flux from low equatorial pitch angles (near the loss cone) as measured at low altitude, to high equatorial pitch angles (far from the loss cone), as necessitated by equatorial flux models. Here we do this using the high energy resolution ELFIN measurements of energetic electrons. Combining those with GPS measurements we develop a model for the electron anisotropy coefficient, , that describes electron flux dependence on equatorial pitch‐angle, , . We then validate this model by comparing its equatorial predictions from ELFIN with in‐situ near‐equatorial measurements from Arase (ERG) in the outer radiation belt.
Misc.
139-
地球電磁気・地球惑星圏学会総会及び講演会(Web), 154th, 2023
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地球電磁気・地球惑星圏学会総会及び講演会(Web), 150th, 2021
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日本地球惑星科学連合大会予稿集(Web), 2020, 2020
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観測ロケットシンポジウム2019 講演集 = Proceedings of Sounding Rocket Symposium 2019, Aug, 2019第2回観測ロケットシンポジウム(2019年8月5日-6日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県著者人数: 15名資料番号: SA6000142020
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宇宙科学技術連合講演会講演集(CD-ROM), 63rd, 2019
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日本地球惑星科学連合大会予稿集(Web), 2019 ROMBUNNO.PEM11‐P24 (WEB ONLY), 2019
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宇宙科学技術連合講演会講演集(CD-ROM), 62nd ROMBUNNO.3C19, 2018
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日本地球惑星科学連合大会予稿集(Web), 2018 ROMBUNNO.PEM15‐21 (WEB ONLY), 2018
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地球電磁気・地球惑星圏学会総会及び講演会(Web), 144th ROMBUNNO.R006‐P29 (WEB ONLY), 2018
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FRONTIERS IN THEORETICAL AND APPLIED PHYSICS/UAE 2017 (FTAPS 2017), 869, 2017
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応用物理学会春季学術講演会講演予稿集(CD-ROM), 63rd ROMBUNNO.20P‐KD‐7, Mar 3, 2016
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宇宙航空研究開発機構研究開発報告 JAXA-RR-, 14(14-009) 151-160, Mar 31, 2015Alpha-ray detector (ARD) onboard SELENE was designed for detecting α-particles emitted by Rn-222 emanated on the lunar surface and its descendent nuclear species Po-210. Distribution and variation of radon gas measured by the α-particle signal is expected to provide information on the subsurface uranium distribution, crustal structures including faults, and behavior of the thin atmosphere of the moon. In this paper, we describe the flow of ARD data processing and a method to derive the α-particle intensity distribution utilizing the angular response of the detector which is applied to the radon α-particle observations for the first time. The method improves the resolution of the α-particle intensity map and enables detailed comparison with the geographical features of the lunar surface.
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日本物理学会講演概要集(CD-ROM), 70(1) ROMBUNNO.21PDD-13-417, Mar 24, 2015
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Development of the high‐speed digital processing system by ASIC for HEP‐e on board the ERG satellite電子情報通信学会技術研究報告, 113(367(SANE2013 107-112)) 7-12, Dec 13, 2013The ERG (Energization and Radiation in Geospace) satellite observes Geospace containing the radiation belt which direct observation was not yet fully conducted, and the elucidation of acceleration mechanism of a relativistic particle in Geospace associated with space storm. The particle observation by ERG satellite employs 6 PPE (Plasma particle Experiment) in total, and HEP-e which is one of the PPE instruments the electron of the range from 0.07 to 2 MeV by SSSD. Finally, we establish calculation process using ASIC called VATA for radiation analysis. This VATA for HEP-e on board the ERG has ADC, which is not used in ASIC for HEP on board MMO, realizing more miniaturization and power-saving. However, we still have not yet fully understood about the processing maximum speed in active. It became clear that ASIG can demonstrate the speed of 5.5 kHz at the latest through this quality assessment. Furthermore, even if low on the whole, it was shown for the first time that it can calculate high energetic electrons with the speed of 1.86 kHz.
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電子情報通信学会技術研究報告, 112(330(SANE2012 110-119)) 41-45, Nov 23, 2012ERG (Energization and Radiation in Geospace) satellite will be launched to study acceleration processes of energetic particles in the radiation belt surrounding the earth. It is very important to reveal the acceleration process of high-energy particles for both science and application to space weather forecast. Drastic increase of high-energy electrons in the radiation belt is sometimes observed during a geomagnetic storm. When a large magnetic storm occurs, energetic electron count rate may exceed flux limit expected in the nominal design and large number of incident electrons leads to detection loss. Purpose of this study is to demonstrate that the count rate range of a single detector on board ERG satellite can be expanded by means of reading circuit operation to decrease an area of detection.
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日本惑星科学会秋期講演会予稿集, 2012 104-104, Oct 24, 2012
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NIRS-M (National Inst. of Radiological Sciences), (251) 243-244, Aug, 2012
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NIRS-M (National Inst. of Radiological Sciences), (244) 258-259, Nov, 2011
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日本惑星科学会秋期講演会予稿集, 2011 125-125, Oct 23, 2011
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2011, Oct 23, 2011
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2010, Oct 6, 2010
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NIRS-M (National Inst. of Radiological Sciences), (234) 272-273, Jun, 2010
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2009 36-36, Sep 28, 2009The next lunar exploration project, 'SELENE-2' is being planned as a successor to 'KAGUYA'. SELENE-2. The mission science objectives being updated are categorized into two groups. The first one is related to identification of the Moon-forming material, and the second one is related to clarification of the relationship between surface dichotomy and deeper structure. In this talk, we report the current status and the science scenario of the mission.
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Abstracts Fall Meeting of the Japanese Society for Planetary Sciences, 2009 35-35, Sep 28, 2009現在、JAXAでは「かぐや」に続く月探査計画として月惑星への着陸および移動探査技術の獲得を主目的としたSELENE-2計画を検討している。日本地球惑星科学連合2009年大会(5月)では、本ミッションの科学目標、搭載機器候補現状、そしてミッションスケジュールの概略について述べた。本講演では連合大会時に発表した予定案も踏まえ、検討進行状況について報告する。
Professional Memberships
5Research Projects
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2023 - Mar, 2028
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2020 - Mar, 2023
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Grants-in-Aid for Scientific Research Fund for the Promotion of Joint International Research (Fostering Joint International Research (B)), Japan Society for the Promotion of Science, Oct, 2018 - Mar, 2021
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (C), Japan Society for the Promotion of Science, Apr, 2018 - Mar, 2021
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2015 - Mar, 2019