Optimization control for the far-distance rapid cooperative rendezvous of spacecraft with different masses

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. The convergent costate vector is obtained using the particle swarm optimization with differential evolution (PSODE) hybr...

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Veröffentlicht in:	Aerospace science and technology Jg. 45; S. 449 - 461
Hauptverfasser:	Feng, Weiming, Zhao, Di, Shi, Lei, Yang, Kun, Zhao, Junfeng
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.09.2015
Schlagworte:	Active–passive rendezvous Algorithms Cooperative rendezvous Fuel consumption Mathematical analysis Optimization Optimization control Particle swarm and differential evolution hybrid algorithm Rendezvous Sequential quadratic programming method Spacecraft Thrust Vectors (mathematics) Particle swarm and differential evolution hybrid algorithm Cooperative rendezvous Sequential quadratic programming method Active–passive rendezvous Optimization control
ISSN:	1270-9638, 1626-3219
Online-Zugang:	Volltext
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