Optimal Rendezvous Guidance with Enhanced Bearings-Only Observability
2015; American Institute of Aeronautics and Astronautics; Volume: 38; Issue: 6 Linguagem: Inglês
10.2514/1.g000822
ISSN1533-3884
Autores Tópico(s)Space Satellite Systems and Control
ResumoNo AccessEngineering NoteOptimal Rendezvous Guidance with Enhanced Bearings-Only ObservabilityJonathan Grzymisch and Walter FichterJonathan GrzymischInstitute of Flight Mechanics and Control, University of Stuttgart, 70569 Stuttgart, Germany and Walter FichterInstitute of Flight Mechanics and Control, University of Stuttgart, 70569 Stuttgart, GermanyPublished Online:20 Apr 2015https://doi.org/10.2514/1.G000822SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Breger L. S. and How J. 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