中国航空学报(英文版)2024,Vol.37Issue(7) :352-374.DOI:10.1016/j.cja.2024.03.013

Novel high-safety aeroengine performance predictive control method based on adaptive tracking weight

Qian CHEN Hanlin SHENG Jie ZHANG Jiacheng LI
中国航空学报(英文版)2024,Vol.37Issue(7) :352-374.DOI:10.1016/j.cja.2024.03.013

Novel high-safety aeroengine performance predictive control method based on adaptive tracking weight

Qian CHEN 1Hanlin SHENG 1Jie ZHANG 2Jiacheng LI1
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作者信息

  • 1. College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • 2. College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
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Abstract

Increasing attention has been attracted to the dynamic performance and safety of advanced performance predictive control systems of the next-generation aeroengine.The latest research demonstrates that Subspace-based Improved Model Predictive Control(SIMPC)can over-come the difficulty in solving the predictive model in MPC/NMPC applications.However,applying constant design parameters cannot maintain consistent control effects in all states.Meanwhile,the designed system relies too much on sensor-measured data,and thus it is difficult to thoroughly val-idate the safety of the system because of its high complexity.This means that any potential hard-ware/software faults will endanger the engine.Therefore,this paper first presents a novel nonlinear mapping relationship to adaptively tune the tracking weight online with the change of Power Lever Angle(PLA)and real-time relative tracking error.Thus,without introducing additional design parameters,an Adaptive Tracking Weight-based SIMPC(ATW-SIMPC)controller is designed to improve the control performance in all operating states effectively.Then,a Primary/Backup Hybrid Control(PBHC)strategy with the ATW-SIMPC controller as the primary system and the traditional speed(Nf)controller as the backup system is proposed to ensure safety.The designed affiliated switching controller and the real-time monitor therein can be used to realize reasonable and smooth switching between primary/backup systems,so as to avoid bump transition.The PBHC system switches to the Nf controller when the ATW-SIMPC controller is wrong because of potential hardware/software faults;otherwise,the ATW-SIMPC controller keeps acting on the engine.The main results prove that the ATW-SIMPC controller with the optimal nonlinear mapping relation-ship,compared with the existing SIMPC controller,uplifts the dynamic control performance by 32%and reduces overshoots to an allowable limit,resulting in a better control effect in full state.The comparison results consistently indicate that the PBHC can guarantee engine safety in occur-rence of hardware/software faults,such as sensor/onboard adaptive model faults.The approach proposed is applicable to the design of a model-based engine intelligent control system.

Key words

Aeroengine/Model predictive control/Hybrid system/Adaptive weight/Safety

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基金项目

National Natural Science Foundation of China(52176009)

National Natural Science Foundation of China(51906103)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量2
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