@inproceedings{oai:jaxa.repo.nii.ac.jp:00014639,
 author = {伊藤, 匡人 and 大内, 弘文 and 藤井, 孝蔵 and 大山, 聖 and 佐藤, 清 and 入門, 朋子 and 林, 光一 and Ito, Masato and Ouchi, Hirofumi and Fujii, Kozo and Oyama, Akira and Sato, Kiyoshi and Irikado, Tomoko and Hayashi, Koichi A.},
 book = {宇宙航行の力学シンポジウム　平成16年度, Symposium on Flight Mechanics and Astrodynamics 2004},
 month = {Mar},
 note = {Efficient and reliable PSP/TSP measurement system has been developed by using Ruthenium(II) complex and poly-IBM-co-TFEM binder and developing associated image data processing software SMAP for wind tunnel tests in small-scale to large-scale wind tunnels. The present PSP measurement system is inexpensive and easy-to-handle because it uses blue LED as light source. The optimal compounding ratio was found to obtain sufficient pressure and temperature sensitivity of PSP and TSP to improve its accuracy and reliability. SMAP is the GUI-based user-friendly free software that enables automated image data post-processing for PSP/TSP measurement. The present PSP/TSP measurement system has been validated by wind tunnel tests in the large-scale transonic/supersonic wind tunnel in ISAS/JAXA. As for wind tunnel tests of a Shuttle-Orbiter model, the image data post-processing has been successfully demonstrated by using image registration with edge detection and local marker detection. The lift force obtained using mapping process of the PSP measurement data generally agreed with the balance measurement data., 資料番号: AA0048089032},
 pages = {124--127},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {ルテニウム錯体系感圧塗料を用いた宇宙往還機模型の力計測},
 year = {2005}
}