Kun Wang;Jianzhong Qiao;Enmei Wang;Jiakun Lei;Weijia Wang;Tao Meng
{"title":"Safe Inspection Tracking Control for a Tumbling Target Under Full State Constraints and Limited Thrust","authors":"Kun Wang;Jianzhong Qiao;Enmei Wang;Jiakun Lei;Weijia Wang;Tao Meng","doi":"10.1109/TAES.2025.3530392","DOIUrl":null,"url":null,"abstract":"This article addresses the inspection tracking control problem for a tumbling target with specific safety requirements, incorporating constraints on position, attitude motion, velocity, angular velocity, and thrust limitations. To tackle this issue, methods for representing full state constraints are proposed. Specifically, attitude motion constraints under various fields of view are expressed through the plane projection, while velocity constraints are approximated using superquadratics. Consequently, position, velocity, attitude, and angular velocity constraints can each be described by a single function using the proposed representation methods. In addition, a safety filter integrated with an extended state observer (ESO) is developed, allowing for the generation of safe thrust commands through quadratic programming (QP). The safety filter incorporates estimation information from the ESO and considers the convergence dynamics of the estimation error, thereby enhancing the system's safety and robustness. Moreover, the concept of dynamic safety margin is introduced, and an improved safety filter is proposed to increase the feasibility of the QP problem. Numerical simulations are conducted to validate the effectiveness of the proposed control framework.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 3","pages":"6822-6838"},"PeriodicalIF":5.7000,"publicationDate":"2025-01-15","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/10843316/","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 addresses the inspection tracking control problem for a tumbling target with specific safety requirements, incorporating constraints on position, attitude motion, velocity, angular velocity, and thrust limitations. To tackle this issue, methods for representing full state constraints are proposed. Specifically, attitude motion constraints under various fields of view are expressed through the plane projection, while velocity constraints are approximated using superquadratics. Consequently, position, velocity, attitude, and angular velocity constraints can each be described by a single function using the proposed representation methods. In addition, a safety filter integrated with an extended state observer (ESO) is developed, allowing for the generation of safe thrust commands through quadratic programming (QP). The safety filter incorporates estimation information from the ESO and considers the convergence dynamics of the estimation error, thereby enhancing the system's safety and robustness. Moreover, the concept of dynamic safety margin is introduced, and an improved safety filter is proposed to increase the feasibility of the QP problem. Numerical simulations are conducted to validate the effectiveness of the proposed control framework.
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.