固定翼飞机自动载体着陆的观察员增强的滑动模式控制
Xu Peng1, Yan Li1, Zhong Wang1
1School of Automation, Northwestern Polytechnical University, 127 Youyi West Road, Beilin District, Xi'an, Shaanxi, 710072, China.
ISA transactions
|November 9, 2025
概括
这项研究引入了用于自动载体着陆的增强滑动模式控制,提高了对干扰的速度和稳定性. 新方法确保了更快的错误收和在具有挑战性的条件下更好的性能.
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
- 机器人技术 机器人技术 机器人技术
背景情况:
- 在自动载体着陆中,直接升降控制 (DLC) 将姿态和轨迹控制脱.
- 现有的DLC方法表现出缓慢的错误收率和对未知的时间变化的干扰的不良稳定性.
研究的目的:
- 为自动载体着陆提出一个观察员增强的滑动模式控制方案.
- 改进跟踪错误的收速度,提高对外部干扰的稳定性.
主要方法:
- 设计了一种非单元快速积分终端滑动模式控制 (NFITSMC) 用于有限时间误差收.
- 将超扭曲算法嵌入到扩展状态观测器中,创建一个超扭曲扩展状态观测器 (STESO) 用于实时干扰估计.
- 将拟议的控制算法应用于自动航母着陆系统.
主要成果:
- NFITSMC确保了追踪错误的有限时间收.
- STESO有效地估计和补偿未知的时间变化的干扰.
- 利亚普诺夫稳定性分析和模拟证实了快速的误差趋同和强大的稳定性.
结论:
- 拟议的观察员增强的滑动模式控制方案在自动载体着陆中实现了所需的性能.
- 该系统在有限时间内展示了快速的错误收和强大的性能,可以应对复杂的时间变化的干扰.
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