Design and Testing of a Low-Order Flight Control System for Quad-Tilt-Wing UAV
2016; American Institute of Aeronautics and Astronautics; Volume: 39; Issue: 10 Linguagem: Inglês
10.2514/1.g001577
ISSN1533-3884
AutoresHironori Totoki, Yoshimasa Ochi, Masayuki Sato, Koji Muraoka,
Tópico(s)Control Systems and Identification
ResumoNo AccessEngineering NoteDesign and Testing of a Low-Order Flight Control System for Quad-Tilt-Wing UAVHironori Totoki, Yoshimasa Ochi, Masayuki Sato and Koji MuraokaHironori TotokiNational Defense Academy, Yokosuka-shi, Kanagawa 239-8686, Japan, Yoshimasa OchiNational Defense Academy, Yokosuka-shi, Kanagawa 239-8686, Japan, Masayuki SatoJapan Aerospace Exploration Agency, Mitaka-shi, Tokyo 181-0015, Japan and Koji MuraokaJapan Aerospace Exploration Agency, Mitaka-shi, Tokyo 181-0015, JapanPublished Online:9 Aug 2016https://doi.org/10.2514/1.G001577SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Anderson S. B., "Historical Overview of V/STOL Aircraft Technology," NASA TM-81280, 1981. Google Scholar[2] Rothhaar P. M., Murphy P. C., Bacon B. J., Gregory I. M., Grauer J. A., Busan R. C. and Croom M. 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