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
Cited by
1 articles.
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