@article{oai:jaxa.repo.nii.ac.jp:00031688,
 author = {遠山, 文雄 and 大西, 信人 and 宮崎, 勝 and TOHYAMA, Fumio and OHNISHI, Nobuhito and MIYAZAKI, Masaru},
 issue = {4_B},
 journal = {東京大学宇宙航空研究所報告},
 month = {Dec},
 note = {In the experiment of K-10-11 rocket, it needed to stop the roll of the rocket. It was controlled the GAH sensor (horizontal component of geomagnetic aspect sensor) to point at a direction of perpendicular to the geomagnetic meridian plane on the rocket position. Output signals of GAH were used to control the rocket's roll by the rocket control systems. This output signal was a zero-cross signal which GAH field changed from minus to plus, and it was amplified to transmit to the rocket control systems. In order to avoid magnetic effects to the sensor, GAH was mounted on a boom with a length of 30 cm and was extended to the out of rocket after the nose cone opening. The magnetic effects from the rocket body and instruments were measured before launching., 資料番号: SA0124693000},
 pages = {999--1003},
 title = {K-10-11号機地磁気姿勢計},
 volume = {12},
 year = {1976}
}