{"title":"Identification of parameters for tethered satellite system to emulate net-captured debris towing","authors":"","doi":"10.1016/j.actaastro.2024.09.022","DOIUrl":null,"url":null,"abstract":"<div><div>Net-based debris capture systems have a high potential for success in Active Debris Removal (ADR) missions. Simulation is an important tool in the analysis of the dynamics of nets, before experiments and actual missions are put in place. However, due to the large number of degrees of freedom required to model the dynamics of a net, in addition to nonlinearities, high-fidelity net-based ADR simulations are typically very computationally costly. This work focuses on the post-capture phase of a net-based ADR mission and aims to identify parameters of a lower-order model of the towed debris system such that it best matches the high-fidelity simulations with a full net. A model of a tethered satellite system with four sub-tethers is developed, and two optimization problems are formulated – minimizing the difference in dynamical quantities of interest – to perform the parameter identification task. The proposed system identification framework is first validated on a benchmark sub-tether model with known parameters, and then employed to minimize the difference in dynamics between the full-net and sub-tether debris towing simulations. The performances of the optimized solutions obtained from two proposed cost functions are compared both qualitatively and quantitatively. Overall, the proposed lower-order modeling and parameter identification framework demonstrate satisfactory performance in approximating the dynamics of the high-fidelity system.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":null,"pages":null},"PeriodicalIF":3.1000,"publicationDate":"2024-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Acta Astronautica","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0094576524005241","RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
Net-based debris capture systems have a high potential for success in Active Debris Removal (ADR) missions. Simulation is an important tool in the analysis of the dynamics of nets, before experiments and actual missions are put in place. However, due to the large number of degrees of freedom required to model the dynamics of a net, in addition to nonlinearities, high-fidelity net-based ADR simulations are typically very computationally costly. This work focuses on the post-capture phase of a net-based ADR mission and aims to identify parameters of a lower-order model of the towed debris system such that it best matches the high-fidelity simulations with a full net. A model of a tethered satellite system with four sub-tethers is developed, and two optimization problems are formulated – minimizing the difference in dynamical quantities of interest – to perform the parameter identification task. The proposed system identification framework is first validated on a benchmark sub-tether model with known parameters, and then employed to minimize the difference in dynamics between the full-net and sub-tether debris towing simulations. The performances of the optimized solutions obtained from two proposed cost functions are compared both qualitatively and quantitatively. Overall, the proposed lower-order modeling and parameter identification framework demonstrate satisfactory performance in approximating the dynamics of the high-fidelity system.
期刊介绍:
Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to:
The peaceful scientific exploration of space,
Its exploitation for human welfare and progress,
Conception, design, development and operation of space-borne and Earth-based systems,
In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.