滑动模式控制与动力类型屏障功能,用于基于干扰观察员的自主空中加油
Jintao Hu1, Yunjie Wu1, Shanwei Su1
1School of Automation Science and Electrical Engineering, Beihang University, Beijing, 100191, China; State Key Laboratory of Virtual Reality Technology and System, Beihang University, Beijing, 100191, China; Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing, 100191, China.
ISA transactions
|October 9, 2025
概括
自主空中加油 (AAR) 面临风暴带来的挑战. 本研究介绍了一种新的干扰拒绝滑动模式控制 (SMC) 策略,使用屏障功能来提高飞机对接的精度和稳定性.
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:
- 自主空中加油 (AAR) 需要精确的控制,特别是在对接期间.
- 突如其来的大气干扰,如风暴,会大大降低控制的准确性和安全性.
研究的目的:
- 开发一个先进的干扰拒绝滑动模式控制 (SMC) 战略,用于接收飞机在AAR.
- 为了提高AAR系统在突发外部干扰下的稳定性和跟踪精度.
主要方法:
- 基于估计器的干扰观察器被开发用于SMC的料补偿和聊天缓解.
- 基于单一功率屏障功能的SMC (SPBFSMC) 已被引入,以快速补偿估计错误.
- 提出了一种基于双功率屏障功能的SMC (DPBFSMC),将两种SPBFSMC方法结合起来,以提高收性和准确性.
主要成果:
- 干扰观察者有效地补偿时间变化的干扰,而不需要事先了解它们的边界.
- SPBFSMC确保了快速收,并避免了在突发干扰下高估收益.
- DPBFSMC实现了较小的最终收区域,显著提高了跟踪准确性.
结论:
- 提出的基于屏障功能的SMC策略提高了AAR控制精度和对突然干扰的稳定性.
- 双重力量的方法提供优越的跟踪准确性,最大限度地减少了融合区域.
- 利亚普诺夫稳定性分析证实了闭环系统的稳定性,并通过模拟验证.
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