DocumentCode
3394071
Title
Stable control for R/C helicopter
Author
Tanaka, Kazuo ; Ohtake, Hiroshi ; Hori, Tsuyoshi
Author_Institution
Dept. of Mech. Eng. & Intelligent Syst., Univ. of Electro-Commun., Chofu, Japan
Volume
4
fYear
2001
fDate
25-28 July 2001
Firstpage
2056
Abstract
This paper presents the stable control for an R/C helicopter whose degree of freedom is reduced by fixing at a (joint) point. The nonlinear model of the R/C helicopter is constructed. After simplifying the nonlinear dynamics, we replace the simplified nonlinear dynamics with a Takagi-Sugeno fuzzy model. The control purpose is to realize good speed of response as well as stabilization with small control effort from practical control points of view. We present a decay rate condition and an input constraint condition that realize good speed of response and avoidance of actuator saturations, respectively. Both of them are represented in terms of linear matrix inequalities. By simultaneously solving them, we design a stable fuzzy controller that achieves good speed of response with small control effort
Keywords
aircraft control; fuzzy control; helicopters; matrix algebra; robust control; R./C helicopter; Takagi-Sugeno model; aircraft control; dynamics; fuzzy control; linear matrix inequality; robust control; stabilization; Actuators; Control systems; Equations; Fuzzy control; Helicopters; Mechanical engineering; Nonlinear systems; Propellers; Stability; Takagi-Sugeno model;
fLanguage
English
Publisher
ieee
Conference_Titel
IFSA World Congress and 20th NAFIPS International Conference, 2001. Joint 9th
Conference_Location
Vancouver, BC
Print_ISBN
0-7803-7078-3
Type
conf
DOI
10.1109/NAFIPS.2001.944386
Filename
944386
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