The problem is considered of spacecraft guidance in the stage of distant approach to an orbital station using the second derivative of relative distance as information about rotation of the line of sight.
Certain Problems of Rendezvous of a Space Vehicle with an Orbital Station
1965
2 pages
Report
No indication
English
Orbital maneuvers and space rendezvous
Online Contents | 2015
|Orbital maneuvers and space rendezvous
Elsevier | 2015
|