@inproceedings{oai:jaxa.repo.nii.ac.jp:00003406,
 author = {鳥居, 弘志 and Torii, Hiroshi},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application},
 month = {Mar},
 note = {First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan, Conventionally flutter boundaries have been predicted based on the modal damping. However, the accurate estimation of damping is difficult and, in some cases, the damping coefficient is not necessarily an appropriate measure for the flutter prediction. To overcome the defect of the damping method, authors proposed an alternative parameter, the flutter margin for discrete-time systems (FMDS), which is approximately equivalent to Zimmermann's flutter margin, and has suitable properties as the flutter prediction parameter. Since it was applicable only to the binary flutter, we have attempted to extend the FMDS so as to be applicable to a higher-mode system. In this paper we give an overview of FMDS and attempt its extension to a higher-mode system., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630046013, レポート番号: JAXA-SP-16-008E},
 pages = {131--140},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Extension of discrete-time flutter prediction method to a higher-mode system},
 volume = {JAXA-SP-16-008E},
 year = {2017}
}