基于干扰排斥的自适应非单元快速终端滑动模式控制,用于四旋翼在强烈的流风下
Armando Miranda-Moya1, Herman Castañeda1, Hesheng Wang2
1Tecnologico de Monterrey, School of Science and Engineering Av. Eugenio Garza Sada 2501 Sur Monterrey, Nuevo, Leon 64849, Mexico.
ISA transactions
|December 19, 2024
概括
本研究介绍了四旋翼无人机的先进控制策略,增强了对抗严重风力干扰的稳定性. 新方法确保了精确的控制,并减少了能源消耗,即使有传感器噪声.
科学领域:
- 机器人和控制系统 机器人和控制系统
- 航空航天工程 航空航天工程
背景情况:
- 四旋翼无人驾驶飞行器 (UAV) 面临着模型不确定性和严重的外部干扰,如风等重大挑战.
- 现有的控制策略往往在精确的状态估计和强大的干扰拒绝方面扎,导致性能下降.
研究的目的:
- 为四旋翼无人机设计一个强大的干扰排斥控制策略.
- 在恶劣的环境条件下提高四旋翼控制系统的稳定性,有限时间收和声减弱.
主要方法:
- 一个扩展状态观察器 (ESO) 已被开发用于实时全状态和总干扰估计.
- 提出了一个具有单增益结构的自适应非单元快速终端滑动模式控制器 (ANFTSMC).
- 使用同质性和利亚普诺夫理论进行了稳定性分析.
主要成果:
- 在一定的时间内,ESO提供了准确的状态和干扰估计,而不考虑最初的错误.
- 该ANFTSMC实现了实际的有限时间收和针对局限外部干扰的稳定性.
- 与现有方法相比,模拟表明干扰的影响较小,扭矩力较低,即使有传感器噪声.
结论:
- 拟议的基于观察者的控制策略有效地提高了四旋翼无人机在模型不确定性和严重风力干扰的情况下的性能.
- 集成的ESO和ANFTSMC提供了一个有前途的解决方案,用于强大的和高效的四旋翼飞行控制.
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