A novel multivariable nonlinear robust control design for turbofan engines

Author:

Cheng Dingding12,Liu Lijun12,Yu Zhen1ORCID

Affiliation:

1. Department of Automation, Xiamen University, China

2. Shenzhen Research Institute of Xiamen University, China

Abstract

Traditional steady-state control methods are applied to turbofan engines operating in the small region near certain operating conditions, which need to switch controllers for operating in the large region and then may lead to instability and performance degradation of the closed-loop system. In this paper, a novel multivariable nonlinear robust control method for turbofan engines is proposed to improve the control performance within the large region. To enlarge the controllable region, a polynomial state-space model describes the nonlinear characteristics of turbofan engines. Based on the analysis of the closed-loop control system, by using the Lyapunov function theorems, a polynomial robust controller is designed to ensure the stability and desired nonlinear control performance of turbofan engines. Compared with the classical PI, mixed sensitivity, and H∞ control, simulation results show that the proposed method has better transient responses, disturbance rejection, and other control performance for the turbofan engine within the large region.

Funder

the Advanced Jet Propulsion Creativity Center, AEAC

Open Foundation of Key Laboratory of Marine Navigation and Control Technology

science and technology foundation of shenzhen city

natural science foundation of fujian province

Publisher

SAGE Publications

Subject

Instrumentation

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