A mathematical model for the optimization of trajectories and, in particular, a stochastic functional depending on the distance between the actual and the assigned trajectory of a dumbbell satellite subjected to a random field of aerodynamical actions in upper-atmosphere flow conditions is proposed. The existence of the minimum of this functional is proved and two simulations are presented by means of a direct method of solution.
|Titolo:||A mathematical model for the motion of a class of dumbbell satellites: stochastic optimization and control of trajectories|
|Data di pubblicazione:||1983|
|Digital Object Identifier (DOI):||10.1016/0270-0255(83)90046-5|
|Appare nelle tipologie:||1.1 Articolo in rivista|