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Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data

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Identiferoai:union.ndltd.org:NAGOYA/oai:ir.nul.nagoya-u.ac.jp:2237/14420
Date08 1900
CreatorsTakahama, Morio, Sakamoto, Noboru, Yamato, Yuhei
PublisherInstitute of Electrical and Electronics Engineers
Source SetsNagoya University
LanguageEnglish
Detected LanguageEnglish
TypeArticle(publisher)
RightsCopyright © 2009 IEEE. Reprinted from (relevant publication info). This material is posted here with permission of the IEEE. Such permission of the IEEE does not in any way imply IEEE endorsement of any of Nagoya University’s products or services. Internal or personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution must be obtained from the IEEE by writing to pubs-permissions@ieee.org.

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