Halo orbit mission correction maneuvers using optimal control
type: Item
instance of: scholarly article
title: Halo orbit mission correction maneuvers using optimal control
zbMATH Open document ID: 1172.93388
DOI: 10.1016/S0005-1098(01)00279-5
author: Radu Serban
author: Martin W. Lo
author: Wang Sang Koon
author: J. E. Marsden
author: Linda Petzold
published in: Automatica
publication date: 2002-09-05T00:00:00Z
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 49N90
zbMATH DE Number: 1797034
zbMATH Keywords: Dynamical systems
zbMATH Keywords: Optimal control
zbMATH Keywords: Halo orbit transfer
zbMATH Keywords: Invariant manifolds
zbMATH Keywords: Three-body problem
zbMATH Keywords: Space mission design
describes a project that uses: ADIFOR
describes a project that uses: DASPK 3.0
describes a project that uses: SNOPT
describes a project that uses: COOPT
MaRDI profile type: Publication
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full work available at URL: s0005-1098(01)00279-5
OpenAlex ID: W2142302039
description: scientific article; zbMATH DE number 1797034