Rate Bumpless Switching Control for Turbofan Control Systems With Actuator Fault Based on Switched Models

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-03-12 DOI:10.1109/TAES.2025.3544599
Yuxuan Gao;Ying Zhao;Rui Wang;Dingyi Huang;Xian Du
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Abstract

This article proposes a rate bumpless switching control approach for the turbofan control systems with actuator faults based on switched models. A characterization of the rate bump restraint is introduced, quantifying the rate bump restraint level based on the state magnitude at the switching points. Unlike the existing description of the rate bumpless switching performance, this description more accurately captures the original intent of bumpless switching. By jointly designing the rate bumpless restriction-dependent switching command and dynamic output feedback control law, a robust stability condition is formulated with the actuator fault addressed. The established rate bumpless switching control method is effectively validated through simulation experiments on the hardware-in-the-loop platform and semiphysical experimental testbed.
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基于切换模型的执行器故障涡扇控制系统速率无颠簸切换控制
针对执行器故障的涡扇控制系统,提出了一种基于切换模型的速率无颠簸切换控制方法。引入了速率碰撞约束的表征,基于开关点的状态大小量化了速率碰撞约束水平。与现有的速率无颠簸开关性能描述不同,这种描述更准确地捕捉了无颠簸开关的初衷。通过联合设计速率无凹凸限制相关切换指令和动态输出反馈控制律,建立了鲁棒稳定条件,解决了执行器故障问题。通过半物理实验平台和硬件在环平台上的仿真实验,有效地验证了所建立的速率无颠簸切换控制方法。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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