Optimization of low-thrust multi-debris removal mission via an efficient approximation model of orbit rendezvous
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DOI: 10.1177/09544100221074746
Abstract: An efficient iterative approximation model for low-thrust rendezvous in low-earth orbit is proposed to be applied in optimization of multi-debris removal missions. Based on an existing method for impulsive orbit rendezvous and a novel iteration… read more here.
Keywords: low thrust; debris removal; orbit rendezvous; approximation model ... See more keywords