DocumentCode
2671547
Title
Robust Takagi-Sugeno fuzzy control for a mini aviation engine
Author
Jinju, Shao ; Minxiang, Wei ; Weidong, Wen
Author_Institution
Coll. of Energy & Power Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
fYear
2008
fDate
16-18 July 2008
Firstpage
775
Lastpage
780
Abstract
A nonlinear speed controller is designed using a fuzzy control strategy based on a Takagi-Sugeno (TS) modelling and robust control approach for a mini unmanned helicopter 2-cylinder, two-stroke, electronic fuel injection engine. A physical nonlinear model of the engine is presented and transformed into an uncertain fuzzy TS model to address the nonlinear system characteristics. Then, a robust nonlinear fuzzy control algorithm is developed via Linear Matrix Inequality (LMI), which can provide reference speed tracking despite the presence of torque load disturbances and operating condition changes. The simulations show that the proposed controller can meet the performance requirements for the unmanned helicopter engine use, namely tracking performance, disturbance rejection and robustness.
Keywords
aerospace engines; angular velocity control; fuzzy control; helicopters; internal combustion engines; linear matrix inequalities; nonlinear control systems; remotely operated vehicles; robust control; LMI; disturbance rejection; electronic fuel injection engine; linear matrix inequality; mini aviation engine; mini unmanned helicopter; nonlinear speed controller; robust Takagi-Sugeno fuzzy control; torque load disturbances; tracking performance; Control systems; Engines; Fuels; Fuzzy control; Fuzzy systems; Helicopters; Nonlinear control systems; Nonlinear systems; Robust control; Takagi-Sugeno model; Engine speed control; LMI; Mini unmanned helicopter; Robust control; Takagi-sugeno models;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location
Kunming
Print_ISBN
978-7-900719-70-6
Electronic_ISBN
978-7-900719-70-6
Type
conf
DOI
10.1109/CHICC.2008.4605819
Filename
4605819
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