概括
本研究介绍了用于航天器态度跟踪的新的有限时间控制器,增强了对干扰的稳定性,并确保了控制扭矩限制. 连续设计是无聊的,通过模拟验证.
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
背景情况:
- 航天器态度跟踪对于任务的成功至关重要.
- 外部干扰和控制输入和带来了重大挑战.
研究的目的:
- 为太空飞船开发强大的,有限时间的态度跟踪控制器.
- 解决外部干扰和输入和问题.
主要方法:
- 在控制器设计中使用后退方法.
- 引入了改进的适应法,以适应干扰的强度.
- 集成的超标功能和辅助系统来处理输入和.
主要成果:
- 设计了两个连续的,无聊的有限时间控制器.
- 证明了对外部干扰的强度.
- 确保的控制扭矩保持在预先确定的范围内.
结论:
- 拟议的有限时间控制策略对于航天器态度跟踪是有效的.
- 控制器提供了更好的稳定性,并处理输入和.
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