日本地球惑星科学連合2024年大会

講演情報

[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

2024年5月30日(木) 17:15 〜 18:45 ポスター会場 (幕張メッセ国際展示場 6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 〜 18:45

[PEM17-P15] Particle-in-Cell Simulations on Interferometry Technique Using Monopole Electric Field Sensors

*深澤 伊吹1三宅 洋平2臼井 英之2栗田 怜3小嶋 浩嗣3 (1.京都大学大学院工学研究科電気工学専攻、2.神戸大学大学院システム情報学研究科、3.京都大学生存圏研究所)

キーワード:干渉計観測、プラズマ波動、PICシミュレーション

One of the principal parameters characterizing plasma waves is their phase velocities. Single-spacecraft interferometry observations can obtain the phase velocities of plasma waves in space. Those observations use the electric field signals picked up by two monopole electric field sensors. The phase velocity is calculated by the phase difference in the waveforms and distance between observation points. However, the complexity of the electric field observations introduced uncertainty. For instance, the distance introduced uncertainty due to the properties of the plasma. Moreover, distortions in the electric field wavefront arise from both the spacecraft body and the electric field sensors themselves. Evaluations based on realistic models of plasma environments are important for obtaining precise phase velocities from observations.
In this study, we use the full-PIC simulation to evaluate the interferometry technique and determine the equivalent length Leq. We perform three-dimensional full particle-in-cell simulations to evaluate the interferometry technique applied to Langmuir waves excited by bump-on-tail instability. The sensor elements in the simulations are simple conductive rods with a particular length. The two waveforms picked up by each monopole sensor provide the time difference. The equivalent distance is calculated using the time difference and the phase velocity for the excited Langmuir waves. The simulation results reveal that the equivalent length for observing the Langmuir waves turns out to be slightly shorter than the sensor’s center-to-center distance. This is considered to be attributed to the distortion of the wavefront by the sensors and the spacecraft.