无人直升机的俯冲角和高度控制基于新的无近距离控制
Haixiang Jiang1, Hao Yang1, Jian Cen1,2
1School of Automation, Guangdong Polytechnic Normal University, Guangzhou 51000, China.
The Review of scientific instruments
|November 15, 2024
概括
本研究提出了一种用于无人直升机的新控制方法,提高了俯冲和高度稳定性. 该技术提高了性能,并且在不需要复杂的计算的情况下处理干扰.
科学领域:
- 机器人技术 机器人技术 机器人技术
- 控制系统工程 控制系统工程
- 航空航天工程 航空航天工程
背景情况:
- 无人直升机需要强大的控制才能稳定飞行.
- 现有的控制方法通常涉及复杂的计算或近似.
- 外部干扰和系统不确定性带来了重大挑战.
研究的目的:
- 引入一种增强的非近似控制技术,用于无人直升机的俯冲和高度.
- 提高过渡和稳定状态响应能力.
- 提供一个计算高效和强大的控制解决方案.
主要方法:
- 将规定的性能控制集成到无人直升机系统中.
- 制定一个非近似的控制策略.
- 使用模拟来验证性能.
主要成果:
- 显著改善过渡和稳定状态响应.
- 有效处理不可预测的外部干扰和系统动态.
- 避免与神经网络和模糊控制相关的计算复杂性.
结论:
- 拟议的非近似控制技术为无人直升机控制提供了简化和强大的解决方案.
- 该方法提高了系统性能,而不依赖于函数近似.
- 它的简单性和效率使它适合于现实世界的应用.
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