基于混合多项式LPV综合的航空发动机增益调度控制

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE International Journal of Turbo & Jet-Engines Pub Date : 2023-01-30 DOI:10.1515/tjj-2023-0001
Bin Shen, Lingfei Xiao, Zhuolin Ye
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引用次数: 1

摘要

本文针对某涡扇发动机,设计了一种基于全包络LMI的多区域线性参数变功率控制器。根据航空发动机模型的特点,首先将三个调度变量分为两组,然后对其中的一部分进行划分,而不是像通常的多区域LPV控制那样直接对所有调度变量进行划分。建立了航空发动机在特定飞行条件下的多项式LPV模型。设计了一种基于参数相关李雅普诺夫函数的显式LPV控制器,并提出了一种消除LPV控制器对调度参数导数依赖性的方法。将涡扇发动机的飞行包络线划分为多个子区域,提出了一种区域重叠的混合LPV控制方法,该方法可以保证整个飞行包络线的稳定性和性能。最后,对一台双轴涡扇发动机非线性部件级模型的仿真结果验证了我们的方法。
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Gain scheduling control of aero-engine based on mixing polynomial LPV synthesis
Abstract A full envelope LMI-based multi-region linear parameter-varying power controller is designed for a turbofan engine in this paper. According to the characteristics of aero-engine model, three scheduling variables are divided into two groups firstly, and then part of them are partitioned, rather than all scheduling variables are partitioned directly as the usual multi-region LPV control. The polynomial LPV model of aero-engine is established under a specific flight condition. An explicit LPV controller by gridding method based on parameter-dependent Lyapunov function is designed and we propose a method to eliminate the dependence of LPV controller on the derivative of scheduling parameter. The flight envelope of turbofan engine is divided into multiple sub-regions, and a mixing LPV control method with overlapping regions is proposed, which can guarantee stability and performance across the full envelope. Finally, the simulation results on the nonlinear component level model of a twin-spool turbofan engine verify our method.
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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