Approximated Closed-Form Solution to Energy-Optimal Satellite Formation Reconfiguration Near Elliptic Orbits
Journal of Guidance, Control, and Dynamics ; 41 , 9 ; 2082-2084
01.09.2018
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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
|