Multi-Input Multi-Output Robust Control of Turbofan Engines Based on Off-Equilibrium Linearization Linear Parameter Varying Model

Author:

Tang Yifeng1,Li Yan2,Yang Wenchong1,Zhou Wenxiang3,Huang Jinquan3,Cui Tao1

Affiliation:

1. School of Aeronautics and Astronautics, Zhejiang University , Zheda Road 38, Hangzhou 310027, China

2. Beijing Power Machinery Research Institute, China Aerospace Science and Industry Corporation , Feihang Road, Beijing 100074, China

3. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics , Yudao Street 29, Nanjing 210016, China

Abstract

Abstract The conventional linear parameter varying (LPV) modeling for turbofan engines is performed at a set of equilibrium points, which may result in inaccurate description of dynamics of engines when the engine accelerates/decelerates in a broad range and operates away from the equilibria. Meanwhile, to ensure stable operation of turbofan engines, the engine pressure ratio (EPR) needs to be regulated when turning on afterburner. According to this complex multi-input multi-output (MIMO) problem mixed with disturbances, this paper proposes a hybrid H∞/H2 robust control framework based on off-equilibrium linearization. We first establish an off-equilibrium linearization based polynomial LPV model for the MIMO turbofan engine, and then design an H∞/H2 robust controller by solving sum-of-squares (SOS) programing. The simulation results show that the controller can simultaneously achieve fast dual command tracking and disturbance suppression when turning on afterburner. Furthermore, this control framework is superior to the equilibrium linearization-based controller in many aspects, which further proves the accuracy of the off-equilibrium based LPV model.

Funder

Ministry of Industry and Information Technology of the People's Republic of China

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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