{"title":"Double-level prescribed performance control for rigid spacecraft attitude tracking under actuator faults","authors":"Qin Huang , Ying Zhang","doi":"10.1016/j.asr.2024.11.070","DOIUrl":null,"url":null,"abstract":"<div><div>The problem of prescribed performance attitude tracking control for rigid spacecraft with external disturbance, inertia uncertainties and actuator faults on special orthogonal group SO(3) is investigated in this paper. With the aid of a novel Lyapunov function, a double-level prescribed performance controller is devised to ensure both attitude and angular velocity tracking errors converge within preset performance boundaries. By applying the suggested controller, the setting time, overshoot and steady-state error of both attitude and angular velocity tracking errors can be regulated by preset performance boundaries getting rid of the initial conditions of the control system. Distinguished from the exist prescribed performance controllers, a stricter performance boundary for angular velocity tracking error can be achieved. For the lumped disturbance which stems from the unknown external disturbance, inertia uncertainties and actuator faults, an extended state observer with linear feedback functions is initially designed to provide an estimation with simple structure. Rigorous proofs within a Lyapunov framework and comparison simulations are presented to demonstrate the effectiveness and superiority of the suggested control strategy.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 4","pages":"Pages 3950-3966"},"PeriodicalIF":2.8000,"publicationDate":"2025-02-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0273117724012018","RegionNum":3,"RegionCategory":"地球科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
引用次数: 0
Abstract
The problem of prescribed performance attitude tracking control for rigid spacecraft with external disturbance, inertia uncertainties and actuator faults on special orthogonal group SO(3) is investigated in this paper. With the aid of a novel Lyapunov function, a double-level prescribed performance controller is devised to ensure both attitude and angular velocity tracking errors converge within preset performance boundaries. By applying the suggested controller, the setting time, overshoot and steady-state error of both attitude and angular velocity tracking errors can be regulated by preset performance boundaries getting rid of the initial conditions of the control system. Distinguished from the exist prescribed performance controllers, a stricter performance boundary for angular velocity tracking error can be achieved. For the lumped disturbance which stems from the unknown external disturbance, inertia uncertainties and actuator faults, an extended state observer with linear feedback functions is initially designed to provide an estimation with simple structure. Rigorous proofs within a Lyapunov framework and comparison simulations are presented to demonstrate the effectiveness and superiority of the suggested control strategy.
期刊介绍:
The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc.
NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR).
All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.