适应性故障耐受性控制与规定的性能为翼微型飞行器
Quanqi Wen1, Haifeng Huang1, Jingyan Qin1
1School of Intelligence Science and Technology, University of Science and Technology Beijing, Beijing, 100083, China; Institute of Artificial Intelligence, University of Science and Technology Beijing, Beijing, 100083, China; Key Laboratory of Intelligent Bionic Unmanned Systems, Ministry of Education, University of Science and Technology Beijing, Beijing, 100083, China.
ISA transactions
|October 23, 2025
概括
本研究介绍了翼微型飞行器 (FWMAV) 的新控制方法,该方法可以在执行器故障的情况下确保准确的飞行性能. 该方法保证追踪错误保持在可靠的机器人操作所规定的范围内.
科学领域:
- 机器人技术 机器人技术 机器人技术
- 控制系统工程 控制系统工程
- 航空航天工程 航空航天工程
背景情况:
- 由于其复杂的动态,翼微型飞行器 (FWMAV) 存在独特的控制挑战.
- 确保FWMAV的强大性能和精确的轨迹跟踪对于其实际应用至关重要.
- 执行器故障可以显著降低FWMAVs的性能和稳定性.
研究的目的:
- 为FWMAVs开发基于模型的控制策略,以保证规定的性能.
- 为了应对FWMAV控制系统中执行器故障的挑战.
- 确保追踪错误在特定范围内在有限时间内趋同.
主要方法:
- 制定一种基于模型的控制方法,其中包含屏障Lyapunov函数.
- 包括Nussbaum功能来处理时间变化的执行器故障.
- 在系统稳定性分析中应用利亚普诺夫稳定性理论.
主要成果:
- 拟议的控制方法有效地限制了飞行状态在规定的性能规格内.
- 时间变化的执行器故障被成功管理,保持系统稳定性.
- 模拟显示了FWMAV在执行器故障条件下强大的轨迹跟踪.
结论:
- 开发的控制策略确保了FWMAV的可靠轨迹跟踪,即使在执行器故障的情况下.
- 该方法符合预先确定的绩效指标,增强FWMAV的运营能力.
- 利亚普诺夫稳定理论证实了拟议的控制系统的稳定性和有效性.
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