@inproceedings{oai:jaxa.repo.nii.ac.jp:00005531,
 author = {得竹, 浩 and 砂田, 茂 and 藤永, 仁 and 大塚, 有企朗 and Tokutake, Hiroshi and Sunada, Shigeru and Fujinaga, Jin and Otsuka, Yukio},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第40回, JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition},
 month = {Feb},
 note = {A new pitch controller for our developed small airplane was designed, and its ability was confirmed by simulation. In the pitch controller, outputs from the MEMS (Micro Electro Mechanical System) flow sensor and the transfer function determined by the results of the wind tunnel tests are used. MEMS technology is a key technology of this pitch controller., 資料番号: AA0063908010, レポート番号: JAXA-SP-07-026E},
 pages = {31--34},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Flow control with pitching motion of UAV using MEMS flow sensors},
 volume = {JAXA-SP-07-026E},
 year = {2008}
}