Accelerated Deorbiting of MEO Satellites Using Low-Thrust Propulsion and Resonant Perturbations

dc.contributor.author	Wang, Chunyu
dc.contributor.author	Huang, Runxiang
dc.contributor.author	Yang, Kun
dc.contributor.author	Feng, Jinglang
dc.contributor.author	Liu, Xiaodong
dc.date.accessioned	2026-08-20T21:15:39Z
dc.date.available	2026-08-20T21:15:39Z
dc.date.copyright	2025/12/27
dc.date.issued	2026
dc.identifier.other	JAEEEZ.ASENG-6751.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl1/handle/yetl/4314195
dc.description.abstract	AbstractIn the medium Earth orbit (MEO) region, lunisolar secular resonances can lead to long-term eccentricity growth over timescales of centuries. To accelerate the orbital decay of end-of-life satellites, this study proposes a strategy that uses low-...
dc.publisher	American Society of Civil Engineers
dc.title	Accelerated Deorbiting of MEO Satellites Using Low-Thrust Propulsion and Resonant Perturbations
dc.type	Journal Article
dc.journal.volume	39
dc.journal.issue	2
dc.journal.title	Journal of Aerospace Engineering
dc.identifier.doi	10.1061/JAEEEZ.ASENG-6751
dc.journal.fristpage	04025142-1
dc.journal.lastpage	04025142-12
dc.page	12
dc.tree	Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002
dc.contenttype	Fulltext