日本地球惑星科学連合2025年大会

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[J] ポスター発表

セッション記号 P (宇宙惑星科学) » P-EM 太陽地球系科学・宇宙電磁気学・宇宙環境

[P-EM17] 宇宙プラズマ科学

2025年5月27日(火) 17:15 〜 19:15 ポスター会場 (幕張メッセ国際展示場 7・8ホール)

コンビーナ:天野 孝伸(東京大学 地球惑星科学専攻)、三宅 洋平(神戸大学大学院システム情報学研究科)、諌山 翔伍(九州大学総合理工学研究院)、梅田 隆行(北海道大学 情報基盤センター)

17:15 〜 19:15

[PEM17-P07] Estimation of spurious electric field components produced by spacecraft charging based on the double probe measurements

*中川 朋子1堀 智昭2笠羽 康正3松田 昇也4笠原 禎也4三好 由純2土屋 史紀3熊本 篤志3新堀 淳樹2松岡 彩子5 (1.東北工業大学、2.名古屋大学宇宙地球環境研究所、3.東北大学、4.金沢大学、5.京都大学)

キーワード:電場観測、ダブルプローブ、磁気圏、光電子、あらせ衛星、衛星電位

Measurements of low-frequency electric field by double probe technique suffer from a spurious electric field component produced by the spacecraft charging and photoelectron cloud whose center is supposed to be shifted from the center of the orbit of the probes toward the sun. The waveforms of the spurious potential difference between the spacecraft and the probes are nearly sinusoidal, so it is not easy to separate them from the natural electric field. Furthermore, the higher harmonics of the waveform are contaminated by the modulation of the probe potential arising from the interaction of photoelectrons between the probe and the spacecraft when the external magnetic field connects them.
In this study, we analyze data from PWE/EFD onboard Arase, and remove the fast, spin-phase dependent variation of probe potential from the waveform, to obtain sinusoidal curve that is supposed to be the sum of the spurious electric field and natural electric field. On the assumption that the natural electric field is perpendicular to the eternal magnetic field and that the spurious electric field is parallel to the direction toward the sun, we can estimate the spurious component only when the eternal magnetic field is parallel to the orbital plane of the probes (the spin plane of the spacecraft). A possible relationship is examined between the spurious electric field component and the spacecraft electric potential, since the spacecraft potential is related with the spacecraft charging due to photoemission, and the photoelectron yield is determined by the solar irradiance and the surface material of the spacecraft, which do not change so abruptly. If we find the relationship, we can estimate the spurious electric field component and subtract it from observation.