适应式内部模型控制,用于具有不稳定的空气动力学负载的灵活机翼
IEEE transactions on cybernetics
|June 5, 2023
概括
本研究介绍了适应性内部模型控制,用于灵活的机翼调节,有效地管理未知的干扰和引用. 适应观察器确保了系统稳定性和准确的跟踪错误控制.
科学领域:
- 控制系统工程 控制系统工程
- 航空航天工程 航空航天工程
- 机器人技术 机器人技术 机器人技术
背景情况:
- 灵活的翅膀易受分布和边界干扰的影响.
- 准确的输出调节对于飞行控制系统至关重要.
- 外系系统的不确定性在控制设计中带来了重大挑战.
研究的目的:
- 开发可适应的内部模型控制,以对灵活的机翼进行可靠的输出调节.
- 为了应对未知的外部系统动态,干扰和引用所带来的挑战.
- 为了确保闭环控制系统的内部对称稳定性.
主要方法:
- 基于观察者的追踪错误反控制的设计,用于已知的外系系统矩阵.
- 针对有未知外系矩阵的系统开发自适应观测器.
- 适应观察员与基于观察员的控制器的集成,以适应输出调节.
主要成果:
- 拟议的自适应观察员确保了观察员错误系统的指数趋同.
- 基于观察者的自适应控制成功地将跟踪错误调节到零.
- 闭环系统在未知的干扰和参考条件下表现出内部非对称稳定性.
结论:
- 适应式内部模型控制为灵活的机翼输出调节提供了强大的解决方案.
- 开发的自适应观察者有效地处理未知的外部系统动态.
- 控制策略在存在不确定性的情况下确保稳定和准确的绩效.
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