@inproceedings{oai:jaxa.repo.nii.ac.jp:00003245,
 author = {甲斐, 大貴 and 杉浦, 裕樹 and 手塚, 亜聖 and Kai, Daiki and Sugiura, Hiroki and Tezuka, Asei},
 book = {宇宙航空研究開発機構特別資料: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium},
 month = {Dec},
 note = {第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-41日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京, 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan, The magnetic suspension and balance system (MSBS) suspending the model against high subsonic flow has been successfully developed at Japan Aerospace Exploration Agency (JAXA). In transonic regime, there are difficulties for MSBS to support the model because aerodynamic force acting on the model increases and its fluctuation also increases accordingly. One of JAXA's MSBS for the 10 cm low speed wind tunnel was modified to improve control system response. A 500 Hz control system with image sensors was developed, and the proportional-integral controller was replaced to proportional-integral-differential controller. In addition, to cope with the larger aerodynamic force, more powerful amplifiers were installed and stronger magnets were also installed in the model. The improved MSBS suspended an ogive-cylinder model with diameter of 10 mm and length of 156 mm up to Mach number of 0.6., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1730011011, レポート番号: JAXA-SP-17-004},
 pages = {83--88},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {高亜音速磁力支持天秤風洞の開発},
 volume = {JAXA-SP-17-004},
 year = {2017}
}