DocumentCode
2044116
Title
Redesign implementation of a nonlinear sampled-data controller for a 3-DOF model helicopter
Author
Takamuku, K. ; Ishitobi, M. ; Kumada, T. ; Nishi, M. ; Kunimatsu, S.
Author_Institution
Dept. of Mech. Syst. Eng., Kumamoto Univ., Kumamoto, Japan
fYear
2011
fDate
13-18 Sept. 2011
Firstpage
1014
Lastpage
1018
Abstract
This paper considers redesign implementation of a nonlinear sampled-data controller for a 3-DOF model helicopter. To improve the control performance, an emulation input is modified by an additional signal. The previous method is based on the Euler approximate model, and the improvement of the control performance cannot be expected. It is shown that the improved Euler model can achieve a better control performance. Since the 3-DOF model helicopter is not decouplable via static state feedback, dynamic state feedback is introduced and a further modification to the redesign input is given.
Keywords
aircraft control; control system synthesis; helicopters; nonlinear control systems; sampled data systems; state feedback; 3DOF model helicopter; Euler approximate model; control performance; dynamic state feedback; nonlinear sampled-data controller redesign; redesign input; static state feedback; Control systems; Emulation; Equations; Helicopters; Mathematical model; Numerical models; Helicopter; Nonlinear systems; Redesign; Sampled-data control;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference (SICE), 2011 Proceedings of
Conference_Location
Tokyo
ISSN
pending
Print_ISBN
978-1-4577-0714-8
Type
conf
Filename
6060657
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