四旋翼无人机的几何态度跟踪控制与自适应扩展状态观察员
Liping Wang1, Jiapeng Chen1, Yuyuan Huang1
1Key Laboratory of Autonomous Systems and Networked Control, Ministry of Education, Unmanned Aerial Vehicle Systems Engineering Technology Research Center of Guangdong, School of Automation Science and Engineering, South China University of Technology, Guangzhou, 510640, China.
ISA transactions
|March 16, 2025
概括
本研究介绍了使用自适应扩展状态观察器 (AESO) 处理未知的干扰和不确定性的四旋翼无人机的新控制方法,以确保稳定的态度跟踪.
科学领域:
- 机器人技术 机器人技术 机器人技术
- 控制系统工程 控制系统工程
- 航空航天工程 航空航天工程
背景情况:
- 四旋翼无人机 (UAV) 需要精确的姿态控制.
- 未知的干扰和系统不确定性对无人机控制系统构成重大挑战.
研究的目的:
- 为四旋翼无人机开发一个几何态度跟踪控制方案.
- 通过使用自适应扩展状态观察器 (AESOs) 来应对未知的干扰和系统不确定性带来的挑战.
主要方法:
- 协调转换以简化AESO错误动态分析.
- 在SO3上开发一个与AESO集成的几何跟踪控制器.
- 分析AESO稳定性和在不确定性下估计的误差.
主要成果:
- 拟议的控制方案保证了跟踪错误的指数趋同到一个有限的集合.
- 适应式扩展状态观察器有效估计系统状态和干扰.
- 通过模拟和实际飞行测试进行验证.
结论:
- 与AESOs一起开发的几何态度跟踪控制方案对四旋翼无人机有效.
- 这种方法提高了对未知的干扰和系统不确定性的稳定性.
- 该方法在现实世界飞行场景中的实际适用性得到了验证.
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