Approximated Closed-Form Solution to Energy-Optimal Satellite Formation Reconfiguration Near Elliptic Orbits
Journal of Guidance, Control, and Dynamics ; 41 , 9 ; 2082-2084
2018-09-01
Article (Journal)
Electronic Resource
English
Analytical solution to optimal relocation of satellite formation flying in arbitrary elliptic orbits
Online Contents | 2013
|Spacecraft Formation Reconfiguration in Elliptic Reference Orbits (AIAA 2013-5241)
British Library Conference Proceedings | 2013
|