Phasing Trajectories to Deploy a Constellation in a Halo Orbit - Collections

＜journal article＞
Phasing Trajectories to Deploy a Constellation in a Halo Orbit

Creator	Author PID 0000-0001-9453-6962 K007735 Creator Name Chen, Hongru 陳, 泓儒チン, オウジュ Affiliation Affiliation Name Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences
Creator	Creator Name Ma, Jian Affiliation Affiliation Name Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences Affiliation Affiliation Name University of Chinese Academy of Sciences
Language	English
Publisher	American Institute of Aeronautics and Astronautics
Date	2017-10
Source Title	Journal of Guidance, Control, and Dynamics
Vol	40
Issue	10
First Page	2662
Last Page	2667
Publication Type	Accepted Manuscript
Access Rights	open access
Related DOI	isVersionOf https://doi.org/10.2514/1.G002518
Related DOI

File	FileType	Size	Views	Description
4481566	pdf	2.12 MB	507

PISSN	0731-5090
EISSN	1533-3884
NCID	AA10626513
Record ID	4481566
Subject Terms	Halo Orbit
	Constellations
	Satellite Constellations
	Earth
	Geometric Dilution of Precision
	Phoebe
	Propulsion System
	Lagrangian Point
	European Space Agency
	Orbit Determination
Type	Engineering Note
Funding Information	Funder Name National Natural Science Foundation of China Award Number 11372311
Funding Information	Funder Name Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences Award Number CSU-QZKT-201711
Created Date	2021.07.09
Modified Date	2022.01.24