In this study, the dynamics equation of orbital elements without singularities is used to describe the far-distance cooperative rendezvous of two spacecraft with different masses.
Optimization control for the far-distance rapid cooperative rendezvous of spacecraft with different masses
2015
Aufsatz (Zeitschrift)
Englisch
Optimal control for far-distance rapid cooperative rendezvous
Online Contents | 2014
|Optimal control for far-distance rapid cooperative rendezvous
Tema Archiv | 2014
|Optimal control for far-distance rapid cooperative rendezvous
SAGE Publications | 2014
|Optimal control of rapid cooperative spacecraft rendezvous with multiple specific-direction thrusts
SAGE Publications | 2020
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