{"title":"Prescribed-Time Chattering-Free Sliding Mode Guidance Law With Terminal Angle Constraint Based on Periodic Delayed Feedback","authors":"Haoyu Zheng;Bin Zhou;Yi Ding;Mingrui Hao","doi":"10.1109/TAES.2024.3449274","DOIUrl":null,"url":null,"abstract":"This article proposes a prescribed-time chattering-free sliding mode guidance law with terminal angle constraint based on periodic delayed feedback. First, a prescribed-time sliding mode guidance law is presented based on a periodic delayed sliding mode surface, which can ensure the prescribed-time convergence of both the line-of-sight angular rate and the line-of-sight angle. Second, a prescribed-time extended state observer is proposed to acquire the precise disturbance estimation within the prescribed settling time. In contrast to other finite-time or fixed-time disturbance observer, the convergence time of the proposed observer is concise and easy for tuning. Finally, by incorporating the estimated disturbance into the original prescribed-time sliding mode guidance law, a composite guidance law with prescribed-time convergence is developed, where chattering is completely eliminated. In particular, the convergence time of the proposed prescribed-time extended state observer and prescribed-time sliding mode guidance law can be arbitrarily assigned and prescribed in advance. A series of numerical simulations are carried out to verify the efficacy of the proposed guidance law.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 1","pages":"932-942"},"PeriodicalIF":5.7000,"publicationDate":"2024-08-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10646474/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
This article proposes a prescribed-time chattering-free sliding mode guidance law with terminal angle constraint based on periodic delayed feedback. First, a prescribed-time sliding mode guidance law is presented based on a periodic delayed sliding mode surface, which can ensure the prescribed-time convergence of both the line-of-sight angular rate and the line-of-sight angle. Second, a prescribed-time extended state observer is proposed to acquire the precise disturbance estimation within the prescribed settling time. In contrast to other finite-time or fixed-time disturbance observer, the convergence time of the proposed observer is concise and easy for tuning. Finally, by incorporating the estimated disturbance into the original prescribed-time sliding mode guidance law, a composite guidance law with prescribed-time convergence is developed, where chattering is completely eliminated. In particular, the convergence time of the proposed prescribed-time extended state observer and prescribed-time sliding mode guidance law can be arbitrarily assigned and prescribed in advance. A series of numerical simulations are carried out to verify the efficacy of the proposed guidance law.
期刊介绍:
IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.