Collision-avoidance strategy for a spinning electrodynamic tether system
作者机构：School of AutomationNorthwestern Polytechnical UniversityXi’an 710129China Institute of IT and CybernaticsSamara National Research UniversitySamara 443086Russia
出 版 物：《Astrodynamics》 (航天动力学（英文）)
年 卷 期：2024年第8卷第2期
页 面：247-259页
核心收录：
学科分类：07[理学] 070202[理学-粒子物理与原子核物理] 0702[理学-物理学]
基 金：the support of the National Natural Science Foundation of China(Grant No.62273277) the Key Research and Development Program of Shaanxi(Grant No.2023-GHZD-32) the Fundamental Research Funds for the Central Universities(Grant No.D5000220031) Russian Foundation for basic research assistance(Grant No.21-51-53002)
主 题：spinning electrodynamic tether systems(SEDTs) collision analysis collision avoidance
摘 要：Spinning electrodynamic tether systems(SEDTs)have promising potential for the active removal of space debris,the construction of observation platforms,and the formation of artificial ***,owing to the survivability problem of long tethers,designing collision-avoidance strategies for SEDTs with space debris is an urgent *** study focuses on the design of collision-avoidance strategies for SEDTs with an electrodynamic force(Ampere force).The relative distance between the debris and the SEDT is first derived,and then two collision-avoidance strategies are proposed according to the two different *** debris collides closer to a lighter subsatellite,a stationary avoidance strategy is proposed to change the spatial position of the subsatellite by adjusting only the angular motion of the tether,which maintains the original orbit of the *** debris collides closer to a heavier main spacecraft,a comprehensive avoidance strategy is proposed to change the spatial position of the SEDT by slightly modifying the orbital height and changing the tether angular motion *** numerical results illustrate that the proposed strategies promptly avoid potential collisions of an SEDT with space debris without significant changes in the orbital parameters of the SEDT.
维普期刊数据库