DocumentCode
529743
Title
2DOF control system design for maneuverability matching and gust disturbance rejection in in-flight simulator MuPAL-α
Author
Ebihara, Yoshio ; Fujiwara, Yoshinori ; Hagiwara, Tomomichi ; Sato, Masayuki
Author_Institution
Dept. of Electr. Eng., Kyoto Univ., Kyoto, Japan
fYear
2010
fDate
18-21 Aug. 2010
Firstpage
524
Lastpage
528
Abstract
Multipurpose aviation laboratory-α (MuPAL-α) is an experimental aircraft developed by the Japan aerospace exploration agency (JAXA). Its one of the most important functions is to realize in-flight simulation, i.e., to simulate maneuverability of other aircraft via practical flight experiments. To achieve the desired maneuverability matching under model uncertainty and gust disturbance, in this paper, we construct reference feedforward type 2DOF (RFF-2DOF) control system. We will show via numerical simulation that satisfactory results are obtained by constructing RFF-2DOF control system.
Keywords
aerospace simulation; control system synthesis; feedforward; numerical analysis; 2DOF control system design; Japan aerospace exploration agency; gust disturbance rejection; in-flight simulator MuPAL-a; maneuverability matching; multipurpose aviation laboratory-α; numerical simulation; practical flight experiment; reference feedforward type 2DOF control system; Adaptive control; Aircraft; Aircraft manufacture; Atmospheric modeling; Control systems; Delay; Feedforward neural networks; 2DOF control system; In-flight simulation; disturbance rejection; maneuverability matching;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference 2010, Proceedings of
Conference_Location
Taipei
Print_ISBN
978-1-4244-7642-8
Type
conf
Filename
5603120
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