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经过修改的超级扭转控制器,用于强大的四旋翼飞行轨迹跟踪和悬空
Kumar Abhinav1, Shashi Ranjan Kumar1
1Department of Aerospace Engineering, IIT Bombay, Powai, Mumbai, 400076, Maharashtra, India.
ISA transactions
|July 31, 2024
概括
这项研究引入了四旋翼的自适应控制,改善了轨迹跟踪和悬浮. 新的动态适应法消除了干扰界限的需要,提高了在现实世界条件下的性能.
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:
- 四旋翼控制需要强大的方法来跟踪轨迹和悬浮.
- 现有的修改后的超扭转控制器需要了解干扰极限.
研究的目的:
- 为四旋翼机开发一种新的自适应控制器.
- 消除在控制器增益适应中对干扰极限的预先了解的需要.
主要方法:
- 提出了一种新的基于适应的修改后的超扭转控制策略.
- 使用动态适应法来调整控制器收益,而无需干扰信息.
- 控制器设计在非线性框架内,避免了四旋翼动力学线性化.
主要成果:
- 数字模拟显示了有效的轨迹跟踪和在干扰下悬浮性能.
- 拟议的控制器与现有修改的超扭转控制方法相比,显示出更高的性能.
- 控制器保持有效性,即使四旋翼状态远远偏离名义值.
结论:
- 拟议的基于适应的修改后的超扭转控制提供了增强的四旋翼飞行轨迹跟踪和悬浮.
- 这种适应性方法为四旋翼控制应用提供了更实用和更强大的解决方案.
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