Di Wang;Fan Zhang;Yifeng Ma;Xinyi Tao;Panfeng Huang
{"title":"Robust MPC Autonomous Landing of Tethered Rover for Asteroids Exploration","authors":"Di Wang;Fan Zhang;Yifeng Ma;Xinyi Tao;Panfeng Huang","doi":"10.1109/TAES.2025.3539637","DOIUrl":null,"url":null,"abstract":"This article proposes an innovative asteroid landing rover, employing a tethered space system, which aims to improve mission success rates and ensure landing safety compared to conventional asteroid detection and landing methods.The irregular shape of the asteroid, resulting in the existence of a complex gravitational field in the surrounding space, which may lead to violent time-varying disturbance. Furthermore, the tethered space system exhibits a strong coupling effect, which leads to large variations in tether tension during landing, with serious consequences for the stability of the system. In this article, a nominal robust model predictive control algorithm is proposed. Through robust state constraints and parameter selection, it ensures recursive feasibility and system stability and has a better robustness to the gravitational field of the asteroid. Considering the strong coupling characteristics caused by the space tether, the tether tension is predictively controlled to ensure the stability during landing and the accuracy of the trajectory tracking. Simulation results show that the system completes the release landing process along the desired trajectory, and also maintains stable tracking of tether length and tension under the complex gravitational field environment of the asteroid.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 3","pages":"7355-7368"},"PeriodicalIF":5.7000,"publicationDate":"2025-03-10","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/10919020/","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 an innovative asteroid landing rover, employing a tethered space system, which aims to improve mission success rates and ensure landing safety compared to conventional asteroid detection and landing methods.The irregular shape of the asteroid, resulting in the existence of a complex gravitational field in the surrounding space, which may lead to violent time-varying disturbance. Furthermore, the tethered space system exhibits a strong coupling effect, which leads to large variations in tether tension during landing, with serious consequences for the stability of the system. In this article, a nominal robust model predictive control algorithm is proposed. Through robust state constraints and parameter selection, it ensures recursive feasibility and system stability and has a better robustness to the gravitational field of the asteroid. Considering the strong coupling characteristics caused by the space tether, the tether tension is predictively controlled to ensure the stability during landing and the accuracy of the trajectory tracking. Simulation results show that the system completes the release landing process along the desired trajectory, and also maintains stable tracking of tether length and tension under the complex gravitational field environment of the asteroid.
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.