高级全驱动系统基于方法的控制器设计,用于飞行模式转换中的尾随人员
IEEE transactions on cybernetics
|December 30, 2025
概括
这项研究引入了风扇驱动尾座的新控制方法,改进了飞行模式的过渡. 先进的高顺序完全执行 (HOFA) 方案确保在干扰下更快,更准确和更稳健的性能.
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:
- 风扇驱动的尾座机具有双模式飞行能力 (旋翼和固定翼).
- 由于干扰和复杂性,飞行模式之间的过渡带来了重大控制挑战.
- 现有的控制方法在模式转换期间难以准确和拒绝干扰.
研究的目的:
- 为了研究一个预定义的时间稳定跟踪控制问题,尾座.
- 开发一个强大的控制器,解决参数不确定性和外部干扰.
- 在飞行模式转换期间增强控制精度,收速度和稳定性.
主要方法:
- 采用了二阶动态模型和高阶完全执行 (HOFA) 系统方法.
- 开发了一种高级强大的控制器,以克服当前过渡控制的局限性.
- 提出了一个新的预定义时间HOFA方案,具有可调节的参数,用于灵活的融合时间调整.
主要成果:
- 与传统方法相比,拟议方案显示了更高的控制精度和更快的趋同.
- 实现了对参数不确定性和外部干扰的更好的稳定性.
- 预定义时间的HOFA框架允许明确调整趋同时间.
结论:
- 新的预定义时间HOFA方案为尾座员飞行模式转换提供了卓越的性能.
- 该框架提供了可调整的融合时间和在不确定性情况下的强有力的保证.
- 这项研究解决了当前后卫控制文献中的关键局限性.
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