Title :
Sliding mode control for turboshaft engine with variable inlet guide vane
Author :
Lingfei Xiao ; Renji Gong ; Xinyu Fan ; Yue Zhu
Author_Institution :
Jiangsu Province Key Lab. of Aerosp. Power Syst., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Abstract :
This paper presented a sliding mode controller based on PID reaching law for turboshaft engine with variable inlet guide vane. After analyzing the physical model and mathematical model of compressor elaborately, component-level model of turboshaft engine is obtained. In order to facilitate the turboshaft engine control system design, small deviation linear model of turboshaft engine is achieved based on the component-level model. Taking the unavoidable uncertainties of turboshaft engine into consideration, sliding mode control method is used to construct controller on the basis of PID reaching law. Simulation results validate the effect of the proposed turboshaft engine modeling method and controller design method.
Keywords :
blades; control system synthesis; jet engines; linear systems; three-term control; variable structure systems; PID reaching law; component-level model; sliding mode control; small deviation linear model; turboshaft engine control system design; variable inlet guide vane; Blades; Educational institutions; Engines; Mathematical model; Sliding mode control; Turbines; Turboshaft engine; sliding mode control; small deviation linear model; variable inlet guide vane;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2014 11th World Congress on
DOI :
10.1109/WCICA.2014.7053380