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
Link To Document :
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