Design and experimental verifications of the high-speed turn flight control of single-rotor helicopters by the combination of the backstepping method and optimal servo system

Aiming at the realization of agile autonomous flight for the extension of the flying range of single-rotor helicopters in the limited flight time, the flight control system design and the control performance verification for the high-speed turn flight are conducted. To achieve the reference followin...

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Bibliographic Details
Main Authors: Daigo FUJIWARA, Takayuki SHIOKAWA
Format: Article
Language:Japanese
Published: The Japan Society of Mechanical Engineers 2017-10-01
Series:Nihon Kikai Gakkai ronbunshu
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/transjsme/83/854/83_17-00087/_pdf/-char/en