以观察员为基础的自适应控制,用于用全功能的多旋翼无人机稳定悬挂有效载荷
Jorge M Arizaga1, Armando Miranda-Moya1, Herman Castañeda1
1Tecnologico de Monterrey, School of Sciences and Engineering, Av. Eugenio Garza Sada 2501 Sur, 64849, Monterrey, Mexico.
这项研究引入了一种适应式滑动模式控制器,用于携带有效载荷的六旋翼无人机. 新型观察器估计了有效载荷运动,减少了振荡,并在扰乱的环境中改善了轨迹跟踪.
科学领域:
- 机器人技术 机器人技术 机器人技术
- 控制系统 控制系统
- 航空航天工程 航空航天工程
背景情况:
- 六直升机无人机 (UAV) 需要精确的轨迹跟踪,特别是在携带有效载荷时.
- 有效载荷的振荡会降低飞行性能和控制精度.
- 传统的控制器与未测量的有效载荷动态和外部干扰作斗争.
研究的目的:
- 开发一款基于观察者的自适应滑动模式控制器,用于六旋翼无人机.
- 在没有专用传感器的情况下,估计和补偿有效载荷运动和外部干扰.
- 为了提高轨迹跟踪性能和减少有效载荷振荡.
主要方法:
- 扩展高增益观测器的设计,用于全态和干扰估计.
- 实现一个自适应的滑动模式控制策略.
- 在控制循环中对估计的干扰进行补偿.
- 使用利亚普诺夫理论进行稳定性分析.
主要成果:
- 有效估计有效载荷运动和系统干扰.
- 有效载荷振荡的显著减少和改进的轨迹跟踪.
- 证明了对边界扰动的强度.
- 与传统方法相比,减少了聊天.
- 在模拟中观察到的更快的有效载荷减压.
结论:
- 拟议的基于观察者的自适应滑动模式控制器提高了六旋翼无人机的性能.
- 控制器有效地管理有效载荷动态和环境干扰.
- 这种方法为载有有效载荷的无人机提供了更好的飞行控制和稳定性.
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