Earth-Moon Triangular Libration Point Spacecraft Formations

2007 ◽  
Vol 44 (3) ◽  
pp. 660-670 ◽  
Author(s):  
Kathryn A. Catlin ◽  
Craig A. McLaughlin
Keyword(s):  
Libration Point ◽  
Triangular Libration Point ◽  
Spacecraft Formations

Low-thrust transfer to the Earth-Moon triangular libration point via horseshoe orbit

2020 ◽  
Vol 177 ◽  
pp. 111-121
Author(s):  
Xingji He ◽  
Yuying Liang ◽  
Ming Xu ◽  
Yaru Zheng
Keyword(s):  
Libration Point ◽  
Low Thrust ◽  
Triangular Libration Point ◽  
The Earth ◽  
Horseshoe Orbit

Deformation of a line-element in the phase space at the triangular libration point

1981 ◽  
Vol 23 (2) ◽  
pp. 131-137 ◽  
Author(s):  
V. Szebehely ◽  
R. McKenzie
Keyword(s):  
Phase Space ◽  
Line Element ◽  
Libration Point ◽  
Triangular Libration Point

Periodic motion around the triangular libration point in the restricted problem of four bodies

1967 ◽  
Vol 72 ◽  
pp. 180 ◽  
Author(s):  
Ronald Kolenkiewicz ◽  
Lloyd Carpenter
Keyword(s):  
Periodic Motion ◽  
Restricted Problem ◽  
Libration Point ◽  
Triangular Libration Point

Design and Control of Libration Point Spacecraft Formations

2004 ◽  
Author(s):  
Samantha Infeld ◽  
Scott Josselyn ◽  
Walter Murray ◽  
Isaac Ross
Keyword(s):  
Libration Point ◽  
Spacecraft Formations ◽  
And Control

scholarly journals A transfer network linking Earth, Moon, and the triangular libration point regions in the Earth-Moon system

2018 ◽  
Vol 62 (7) ◽  
pp. 1826-1852 ◽  
Author(s):  
Lucia R. Capdevila ◽  
Kathleen C. Howell
Keyword(s):  
Libration Point ◽  
Moon System ◽  
Triangular Libration Point ◽  
The Earth

scholarly journals An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations

2012 ◽  
Vol 2012 ◽  
pp. 1-14
Author(s):  
Laura Garcia-Taberner ◽  
Josep J. Masdemont
Keyword(s):  
Variational Method ◽  
Libration Point ◽  
Time Interval ◽  
Adaptive Remeshing ◽  
Local Solutions ◽  
Spacecraft Formations ◽  
Maneuvering Spacecraft

We consider a methodology to optimally obtain reconfigurations of spacecraft formations. It is based on the discretization of the time interval in subintervals (called the mesh) and the obtainment of local solutions on them as a result of a variational method. Applied to a libration point orbit scenario, in this work we focus on how to find optimal meshes using an adaptive remeshing procedure and on the determination of the parameter that governs it.

Control of orientation for spacecraft formations in the vicinity of the Sun-Earth L2 libration point

2014 ◽  
Vol 57 (9) ◽  
pp. 1778-1787 ◽  
Author(s):  
Rui Qi ◽  
ShiJie Xu ◽  
Tong Chen
Keyword(s):  
Libration Point ◽  
The Sun ◽  
Spacecraft Formations
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