{"title":"Non-overshooting Fixed Time Control of Free-Flying Space Robotic Manipulators with output constraints: An Inverse Optimal Approach","authors":"Zhicheng Xie, Xianliang Chen, Jiashu Wu, Xiaofeng Wu","doi":"10.1016/j.ast.2025.110079","DOIUrl":null,"url":null,"abstract":"<div><div>Inverse Optimal Control (IOC) features addressing optimal control problem without the need to solve the complex Hamilton-Jacobi-Bellman (HJB) equation. Although IOC has been extensively studied over the recent years, the state of the art lacks the results of achieving a fixed time non-overshooting response with constrained outputs on IOC schemes. In this paper, an adaptive inverse optimal control scheme is proposed to address the tracking problem of free-flying space robotic manipulators subject to system uncertainties and unknown disturbances, which achieves the practical fixed time non-overshooting response with the constrained tracking errors. More precisely, a novel practical fixed time non-singular virtual controller is designed to define the desired dynamics of tracking errors, which features the non-singular <span><math><msup><mrow><mi>n</mi></mrow><mrow><mi>t</mi><mi>h</mi></mrow></msup></math></span> derivative where <span><math><mi>n</mi></math></span> is any positive integers defined by users. Then, an auxiliary variable is designed to work with the virtual controller to guarantee the absence of overshoot even the system is subject to uncertainties and disturbances. After that, a Fixed Time Disturbance Observer (FTDO) based inverse optimal control scheme is finally constructed to achieve a practical fixed time non-overshooting response with the satisfied output constraints. To the best of author's knowledge, this is the first work of simultaneously achieving non-overshooting response, practical fixed time stability, inverse optimality, and constrained output. The stability of the proposed controller is proven by Lyapunov theory, and the effectiveness is verified by numerical simulations.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"161 ","pages":"Article 110079"},"PeriodicalIF":5.0000,"publicationDate":"2025-02-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825001506","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
Inverse Optimal Control (IOC) features addressing optimal control problem without the need to solve the complex Hamilton-Jacobi-Bellman (HJB) equation. Although IOC has been extensively studied over the recent years, the state of the art lacks the results of achieving a fixed time non-overshooting response with constrained outputs on IOC schemes. In this paper, an adaptive inverse optimal control scheme is proposed to address the tracking problem of free-flying space robotic manipulators subject to system uncertainties and unknown disturbances, which achieves the practical fixed time non-overshooting response with the constrained tracking errors. More precisely, a novel practical fixed time non-singular virtual controller is designed to define the desired dynamics of tracking errors, which features the non-singular derivative where is any positive integers defined by users. Then, an auxiliary variable is designed to work with the virtual controller to guarantee the absence of overshoot even the system is subject to uncertainties and disturbances. After that, a Fixed Time Disturbance Observer (FTDO) based inverse optimal control scheme is finally constructed to achieve a practical fixed time non-overshooting response with the satisfied output constraints. To the best of author's knowledge, this is the first work of simultaneously achieving non-overshooting response, practical fixed time stability, inverse optimality, and constrained output. The stability of the proposed controller is proven by Lyapunov theory, and the effectiveness is verified by numerical simulations.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.