Periodic Event-Triggered and Self-Triggered Control of Spacecraft Rendezvous System With Input Delay

IF 6.4 2区 计算机科学 Q1 AUTOMATION & CONTROL SYSTEMS IEEE Transactions on Automation Science and Engineering Pub Date : 2024-08-12 DOI:10.1109/TASE.2024.3439009
Kai Zhang;Meilin Li;Zhijian Hu;Xuefei Yang;Kang-Kang Zhang
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Abstract

This paper solves the problem of spacecraft rendezvous with input delay by designing the periodic event-triggered control (PETC) and periodic self-triggered control (PSTC), respectively. Firstly, a PETC based on the discrete-time parametric Lyapunov equation (DPLE) is designed to stabilize the delayed spacecraft rendezvous systems. Moreover, in order to avoid monitoring the measurement errors, a PSTC algorithm that the updates of the next control law depend on the previous triggered states is also designed. Specially, by using the properties of the DPLE, this new approach is not only simple, but also provides an easy and explicit condition on the only parameter of DPLE to guarantee the non-triviality of the designed PETC and PSTC. Finally, the effectiveness of theoretical results is verified by simulations. Note to Practitioners—Although this paper was inspired by the problem of spacecraft rendezvous, the designed algorithms can also be applied to other time-delay systems. Existing general event-triggered control methods have been used to solve the problem of spacecraft rendezvous for reducing the communication load, although this often complicates the design of the controller due to preventing the occurrence of Zeno phenomenon. To overcome this drawback, This paper proposes a periodic event-triggered control to achieve the spacecraft rendezvous with input delay, which naturally avoids the occurrence of Zeno phenomenon. In addition, a periodic self-triggered control is also designed, which has never been designed to solve the problem of delayed spacecraft rendezvous.
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有输入延迟的航天器会合系统的周期性事件触发和自触发控制
本文通过设计周期事件触发控制(PETC)和周期自触发控制(PSTC)分别解决了具有输入延迟的航天器交会问题。首先,设计了一种基于离散参数李雅普诺夫方程(DPLE)的航天器延迟交会系统的PETC。此外,为了避免监测测量误差,还设计了一种基于前一个触发状态更新下一个控制律的PSTC算法。特别地,利用DPLE的特性,该方法不仅简单,而且为DPLE的唯一参数提供了一个简单明确的条件,以保证所设计的PETC和PSTC的非平凡性。最后,通过仿真验证了理论结果的有效性。虽然本文的灵感来自航天器交会问题,但所设计的算法也可以应用于其他时滞系统。现有的一般事件触发控制方法已被用于解决航天器交会问题,以减少通信负荷,但由于防止芝诺现象的发生,这往往使控制器的设计复杂化。为了克服这一缺点,本文提出了一种具有输入延迟的周期事件触发控制来实现航天器交会,从而自然地避免了芝诺现象的发生。此外,还设计了一种从未设计过的周期自触发控制,用于解决航天器交会延迟问题。
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来源期刊
IEEE Transactions on Automation Science and Engineering
IEEE Transactions on Automation Science and Engineering 工程技术-自动化与控制系统
CiteScore
12.50
自引率
14.30%
发文量
404
审稿时长
3.0 months
期刊介绍: The IEEE Transactions on Automation Science and Engineering (T-ASE) publishes fundamental papers on Automation, emphasizing scientific results that advance efficiency, quality, productivity, and reliability. T-ASE encourages interdisciplinary approaches from computer science, control systems, electrical engineering, mathematics, mechanical engineering, operations research, and other fields. T-ASE welcomes results relevant to industries such as agriculture, biotechnology, healthcare, home automation, maintenance, manufacturing, pharmaceuticals, retail, security, service, supply chains, and transportation. T-ASE addresses a research community willing to integrate knowledge across disciplines and industries. For this purpose, each paper includes a Note to Practitioners that summarizes how its results can be applied or how they might be extended to apply in practice.
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