{"title":"Analytic solution for combined in-plane and out-of-plane spacecraft formation reconfiguration with passive collision avoidance","authors":"Chenglong Xu , Chengxi Zhang , Jihe Wang","doi":"10.1016/j.actaastro.2024.11.024","DOIUrl":null,"url":null,"abstract":"<div><div>Passive collision avoidance mechanism are effective for ensuring the safety of spacecraft formations during the reconfiguration process. This paper investigates the combined in-plane and out-of-plane formation reconfiguration, while incorporating passive collision avoidance constraints. We design a low-collision-risk impulsive maneuver sequence using the relative Eccentricity/Inclination (E/I) vectors theory and conduct a comprehensive passive safety analysis. Furthermore, we introduce an analytic, passively collision-free maneuver strategy by deriving constraint-satisfying solutions for the relative E/I vectors reconfiguration path. For the first time, our approach achieves theoretical completeness in passive collision avoidance, significantly enhancing the safety of transition configurations compared with existing analytic solutions. Finally, simulations results show that our approach offers substantial improvements in reconfiguration passive safety while incurring negligible additional fuel consumption in comparison to existing solution.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":"226 ","pages":"Pages 48-59"},"PeriodicalIF":3.1000,"publicationDate":"2024-11-20","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/S0094576524006714","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
Passive collision avoidance mechanism are effective for ensuring the safety of spacecraft formations during the reconfiguration process. This paper investigates the combined in-plane and out-of-plane formation reconfiguration, while incorporating passive collision avoidance constraints. We design a low-collision-risk impulsive maneuver sequence using the relative Eccentricity/Inclination (E/I) vectors theory and conduct a comprehensive passive safety analysis. Furthermore, we introduce an analytic, passively collision-free maneuver strategy by deriving constraint-satisfying solutions for the relative E/I vectors reconfiguration path. For the first time, our approach achieves theoretical completeness in passive collision avoidance, significantly enhancing the safety of transition configurations compared with existing analytic solutions. Finally, simulations results show that our approach offers substantial improvements in reconfiguration passive safety while incurring negligible additional fuel consumption in comparison to existing solution.
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.