垂直起飞和降落飞机的轨迹跟踪滑动模式控制基于双循环和全球利普希茨稳定性
1Wuxi Vocational College of Science and Technology, Wuxi, Jiangsu, China.
PloS one
|February 7, 2025
概括
本研究介绍了一种用于垂直起降 (VTOL) 飞机的双环滑动模式控制 (SMC) 策略. 新方法确保了强大的稳定性和在复杂的环境中提高了性能.
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
背景情况:
- 垂直起降 (VTOL) 飞机对于城市空中交通,应急响应和灾害监测至关重要,因为它们在狭窄的空间中具有机动性.
- 在VTOLs的双循环控制系统中实现绝对稳定是具有挑战性的,因为循环间跟踪错误会影响整体性能.
研究的目的:
- 为VTOL飞机提出一个优化的双环滑动模式控制 (SMC) 战略.
- 为了解决影响外部循环稳定性的内循环跟踪错误引起的性能下降.
主要方法:
- 在动态系统中利用全球非对称稳定性定理.
- 开发一个具有全球利普希茨连续性的闭环系统,以确保在两个控制循环中的稳定性.
主要成果:
- 拟议的SMC战略保证了内部和外部控制循环的稳定性.
- 该方法在复杂的动态条件下提高了系统的可靠性和灵活性.
- 数字模拟证实了VTOL系统的改进性能和适应性.
结论:
- 双环SMC战略显著提高了运营稳定性,并减少了VTOL模型中的跟踪错误.
- 该方法提高了在具有挑战性的环境中VTOL控制系统的整体弹性和性能.
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