@article{oai:jaxa.repo.nii.ac.jp:00032910,
 author = {湯元, 清文 and 斎藤, 尚生 and 中川, 朋子 and 平尾, 邦雄 and 青山, 巌 and 瀬戸, 正弘 and YUMOTO, Kiyohumi and SAITO, Takao and NAKAGAWA, Tomoko and HIRAO, Kunio and AOYAMA, Iwao and SETO, Masahiro},
 journal = {宇宙科学研究所報告. 特集: 太陽風と彗星の相互作用研究報告},
 month = {Sep},
 note = {「さきがけ」に搭載されたリングコア磁力計は, Halley彗星最接近時の磁場変化や微小IMF変動を成功裡に観測した。この日本初の深宇宙探査機に搭載する為に, 計画的な地上, 大気球, ロケット実験がなされた。これらの研究から, 飛翔体を用いた磁場測定における磁力計設計製作において次の五項目;(1) 磁力計自体の電気的精度, (2) 検出器の機械精度, (3) 飛翔体の磁気バイアス, (4) 飛翔体の姿勢精度, (5) データ伝送量に留意し, 総合的な性能に仕上げる必要があることが確認された。, Sakigake, the first Japanese artificial planet, was launched on 8 January 1985,and passed through the upstream region of comet Halley on 11 March 1986. The ring-core magnetometer carried by Sakigake has successfully detected clear multiple crossings of the helio neutral sheet and the interplanetary magnetic field (IMF) variations. The installed magnetometer had been improved to measure the smaller IMF intensity of ∿5nT. In the design of the magnetometer system, high fidelity of the magnetometer on board the spacecraft had to be examined with respect to following five problems : (1) electrical exactitude of the basic magnetometer, (2) alignment stability of the triaxial sensor assembly, (3) residual magnetism of the spacecraft, (4) stability of the spacecraft oscillation, and (5) capacity of telemetering of scientific data., 資料番号: SA0166719000},
 pages = {45--57},
 title = {「さきがけ」搭載リングコア磁力計について},
 volume = {15},
 year = {1986}
}