{"title":"存在不确定性和输入饱和的高超声速飞行器非奇异柔性预定性能跟踪控制","authors":"Yingtao Liu, Ruisheng Sun, Yu Lu, Wei Chen","doi":"10.1016/j.conengprac.2025.106591","DOIUrl":null,"url":null,"abstract":"<div><div>Existing prescribed performance control methods encounter substantial challenges in effectively handling singularities under both actuator saturation and non-saturation conditions. In addition, current prescribed performance functions are highly sensitive to unknown initial tracking errors, which significantly restricts their applicability. To address these limitations, this article devises a novel and adaptable prescribed performance control scheme tailored for hypersonic vehicles, taking full account of system uncertainties and actuator saturation. Firstly, a pliable prescribed performance function (PPPF) is proposed. This function is capable of accommodating arbitrary initial tracking errors and achieving envelope adjustment independent of control input, thereby enhancing the control system’s adaptability to various initial conditions. Secondly, a new predefined-time convergence mechanism is developed and incorporated into the design of an anti-saturation compensator. This not only stabilizes the saturated system but also improves the convergence performance of auxiliary variable after the saturation subsides. Thirdly, a command filtered backstepping controller is designed for each subsystem of the hypersonic vehicle. In the altitude subsystem, the new convergence mechanism is extended to derive a predefined-time filter (PTF). Unlike existing filters, the PTF can offer superior tracking performance for filtered signals, further optimizing the overall control performance of the system. Finally, the effectiveness and superiority of the proposed control scheme are rigorously validated through numerical simulations and experiments conducted on a turntable servo system. The results demonstrate that the proposed method can significantly improve the control performance of the hypersonic vehicles under complex conditions, providing a reliable and efficient control solution for practical engineering applications.</div></div>","PeriodicalId":50615,"journal":{"name":"Control Engineering Practice","volume":"165 ","pages":"Article 106591"},"PeriodicalIF":4.6000,"publicationDate":"2025-10-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Nonsingular pliable prescribed performance tracking control for hypersonic flight vehicles in the presence of uncertainties and input saturation\",\"authors\":\"Yingtao Liu, Ruisheng Sun, Yu Lu, Wei Chen\",\"doi\":\"10.1016/j.conengprac.2025.106591\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Existing prescribed performance control methods encounter substantial challenges in effectively handling singularities under both actuator saturation and non-saturation conditions. In addition, current prescribed performance functions are highly sensitive to unknown initial tracking errors, which significantly restricts their applicability. To address these limitations, this article devises a novel and adaptable prescribed performance control scheme tailored for hypersonic vehicles, taking full account of system uncertainties and actuator saturation. Firstly, a pliable prescribed performance function (PPPF) is proposed. This function is capable of accommodating arbitrary initial tracking errors and achieving envelope adjustment independent of control input, thereby enhancing the control system’s adaptability to various initial conditions. Secondly, a new predefined-time convergence mechanism is developed and incorporated into the design of an anti-saturation compensator. This not only stabilizes the saturated system but also improves the convergence performance of auxiliary variable after the saturation subsides. Thirdly, a command filtered backstepping controller is designed for each subsystem of the hypersonic vehicle. In the altitude subsystem, the new convergence mechanism is extended to derive a predefined-time filter (PTF). Unlike existing filters, the PTF can offer superior tracking performance for filtered signals, further optimizing the overall control performance of the system. Finally, the effectiveness and superiority of the proposed control scheme are rigorously validated through numerical simulations and experiments conducted on a turntable servo system. The results demonstrate that the proposed method can significantly improve the control performance of the hypersonic vehicles under complex conditions, providing a reliable and efficient control solution for practical engineering applications.</div></div>\",\"PeriodicalId\":50615,\"journal\":{\"name\":\"Control Engineering Practice\",\"volume\":\"165 \",\"pages\":\"Article 106591\"},\"PeriodicalIF\":4.6000,\"publicationDate\":\"2025-10-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Control Engineering Practice\",\"FirstCategoryId\":\"94\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0967066125003533\",\"RegionNum\":2,\"RegionCategory\":\"计算机科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"AUTOMATION & CONTROL SYSTEMS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Control Engineering Practice","FirstCategoryId":"94","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0967066125003533","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
Nonsingular pliable prescribed performance tracking control for hypersonic flight vehicles in the presence of uncertainties and input saturation
Existing prescribed performance control methods encounter substantial challenges in effectively handling singularities under both actuator saturation and non-saturation conditions. In addition, current prescribed performance functions are highly sensitive to unknown initial tracking errors, which significantly restricts their applicability. To address these limitations, this article devises a novel and adaptable prescribed performance control scheme tailored for hypersonic vehicles, taking full account of system uncertainties and actuator saturation. Firstly, a pliable prescribed performance function (PPPF) is proposed. This function is capable of accommodating arbitrary initial tracking errors and achieving envelope adjustment independent of control input, thereby enhancing the control system’s adaptability to various initial conditions. Secondly, a new predefined-time convergence mechanism is developed and incorporated into the design of an anti-saturation compensator. This not only stabilizes the saturated system but also improves the convergence performance of auxiliary variable after the saturation subsides. Thirdly, a command filtered backstepping controller is designed for each subsystem of the hypersonic vehicle. In the altitude subsystem, the new convergence mechanism is extended to derive a predefined-time filter (PTF). Unlike existing filters, the PTF can offer superior tracking performance for filtered signals, further optimizing the overall control performance of the system. Finally, the effectiveness and superiority of the proposed control scheme are rigorously validated through numerical simulations and experiments conducted on a turntable servo system. The results demonstrate that the proposed method can significantly improve the control performance of the hypersonic vehicles under complex conditions, providing a reliable and efficient control solution for practical engineering applications.
期刊介绍:
Control Engineering Practice strives to meet the needs of industrial practitioners and industrially related academics and researchers. It publishes papers which illustrate the direct application of control theory and its supporting tools in all possible areas of automation. As a result, the journal only contains papers which can be considered to have made significant contributions to the application of advanced control techniques. It is normally expected that practical results should be included, but where simulation only studies are available, it is necessary to demonstrate that the simulation model is representative of a genuine application. Strictly theoretical papers will find a more appropriate home in Control Engineering Practice''s sister publication, Automatica. It is also expected that papers are innovative with respect to the state of the art and are sufficiently detailed for a reader to be able to duplicate the main results of the paper (supplementary material, including datasets, tables, code and any relevant interactive material can be made available and downloaded from the website). The benefits of the presented methods must be made very clear and the new techniques must be compared and contrasted with results obtained using existing methods. Moreover, a thorough analysis of failures that may happen in the design process and implementation can also be part of the paper.
The scope of Control Engineering Practice matches the activities of IFAC.
Papers demonstrating the contribution of automation and control in improving the performance, quality, productivity, sustainability, resource and energy efficiency, and the manageability of systems and processes for the benefit of mankind and are relevant to industrial practitioners are most welcome.