Earth-Moon Triangular Libration Point Spacecraft Formations

2007 ◽  
Vol 44 (3) ◽  
pp. 660-670 ◽  
Author(s):  
Kathryn A. Catlin ◽  
Craig A. McLaughlin
2020 ◽  
Vol 177 ◽  
pp. 111-121
Author(s):  
Xingji He ◽  
Yuying Liang ◽  
Ming Xu ◽  
Yaru Zheng

2012 ◽  
Vol 2012 ◽  
pp. 1-14
Author(s):  
Laura Garcia-Taberner ◽  
Josep J. Masdemont

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.


Sign in / Sign up

Export Citation Format

Share Document