结构化的H∞飞行控制器的设计:被动的容错与基于观察者的结构相比
Masayuki Sato1, Andrés Marcos2, Daisuke Akasaka3
1Faculty of Advanced Science and Technology, Kumamoto University, 2-39-1 Kurokami, Kumamoto 860-8555, Japan.
ISA transactions
|September 10, 2023
概括
本研究介绍了飞机的新型耐故障飞行控制系统. 这些先进的控制器提高了安全性和性能,在真正的研究飞机上得到了验证.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统理论 控制系统理论
- 耐故障控制控制的控制方式
背景情况:
- 飞机控制系统需要强大的容错性,以确保安全.
- 现有系统可能无法充分解决执行器故障,如效率丧失 (LOE).
- 需要先进的控制设计方法来提高可靠性.
研究的目的:
- 设计和验证两个新的耐故障飞行控制器架构.
- 实现对纵向和横向方向运动的被动和主动故障容忍,分别.
- 在各种故障和环境条件下评估控制器性能.
主要方法:
- 结构化H∞设计用于纵向控制中的被动故障容忍.
- 基于观察者的主动故障容忍设计,用于横向方向控制.
- 使用 hinfstruct 和 systune 命令进行控制器增益优化.
- 模拟未模拟的动态,使用不确定的有限时间延迟.
- 飞机在循环 (AIL) 测试用于验证.
主要成果:
- 成功设计和验证的被动和主动故障耐受控制器.
- 在JAXA的MuPAL-α研究飞机上展示了控制器的实用性和性能.
- 在无风和有风的条件下验证的性能.
- 已达到7-8的技术准备水平 (TRL).
结论:
- 拟议的飞行控制结构为其有效性和实用性提供了高度的信心.
- 开发的控制器有效地管理执行器故障并确保稳定的飞行.
- 这项研究促进了对耐故障系统的准备,以适用于真实世界的航空应用.
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