通过内部和外部环滑动模式设计,增强了航天器的姿态跟踪控制
1Hunan Mechanical and Electrical Ploytechnic, Changsha, Hunan, China.
PloS one
|July 17, 2025
概括
这项研究引入了一个强大的双循环控制器,用于太空船的态度调节. 集成的滑动模式控制确保了航天器准确和稳定的定向,提高了任务安全性.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统理论 控制系统理论
- 机器人技术 机器人技术 机器人技术
背景情况:
- 航天器态度控制系统 (ACS) 对于任务的成功和安全至关重要.
- 传统的ACS方法在实现高精度和稳定性方面面临挑战.
研究的目的:
- 开发和验证一种新的双循环滑动模式可变结构控制 (SMC) 方法,用于太空飞船态度调节.
- 为了提高航天器姿态控制的准确性,稳定性和稳定性.
主要方法:
- 实现双循环控制架构,其中有一个外部位置循环和一个内部速度循环.
- 使用整体滑动模式控制 (SMC) 设计可靠的开关功能.
- 内部速度循环的更快的融合,以确保整体系统的稳定性.
主要成果:
- 数字模拟证明了拟议的双循环SMC战略的有效性.
- 控制方法实现了精确的航天器姿态调节和稳定的性能.
- 该系统在模拟条件下表现出强性.
结论:
- 拟议的双循环集成SMC为航天器态度控制提供了一个有前途的解决方案.
- 该战略提高了航空航天应用中的任务准确性和安全性.
- 进一步的研究和现实世界的测试是有必要的.
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