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Updated: Jun 3, 2025

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干扰 坚固态度 多旋转机的稳定与控制时刻 陀螺旋
Youyoung Yang1, Sungsu Kim1, Kwanghyun Lee1
1MOASOFT Co., Ltd., Seoul 05770, Republic of Korea.
Sensors (Basel, Switzerland)
|January 8, 2025
概括
这项研究引入了一种新的控制系统,用于多旋转机无人机使用控制时刻旋转机 (CMGs) 和干扰稳定驱动法 (DRDL). 该框架增强了立场稳定,特别是对抗风力干扰,提高了无人机的可靠性.
科学领域:
- 机器人技术 机器人技术 机器人技术
- 航空航天工程 航空航天工程
- 控制系统 控制系统
背景情况:
- 多旋翼无人机由于风等外部干扰而难以稳定姿势.
- 单独的旋转推力通常不足以在具有挑战性的环境中进行强大的控制.
研究的目的:
- 开发一种新的控制框架,以加强多旋翼无人机的姿态稳定.
- 改进无人机控制系统中的干扰拒绝和奇点避免.
主要方法:
- 集成控制时刻旋转机 (CMG) 进行强大的态度控制.
- 快速终端滑动模式控制 (FTSMC) 的应用,用于有限时间的融合.
- 实施干扰稳健驱动法 (DRDL) 以避免奇点.
主要成果:
- 拟议的基于CMG的框架与DRDL在模拟中显示了快速的态度趋同.
- 该系统有效地减少了电机转速和CMG杆运动中的振荡.
- 与伪反向对照相比,观察到避免奇点和减轻干扰的显著改善.
结论:
- 新的控制框架提高了多旋翼无人机的稳定性和可靠性.
- 该方法显示了在苛刻,受干扰的操作环境中实现高性能控制的潜力.
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