In this study, a redesign of a nano-satellite star tracker for operation at high slew rates is investigated. Small agile spacecraft often require a few arc second-accuracy attitude estimation for slew rates up to 15°/s. This paper develops a technology road-map to evolve a new generation of star trackers that are capable of estimating absolute attitude at high slew rates.
Enabling technologies for high slew rate star trackers
01.03.2017
756233 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Online Contents | 1995
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NTRS | 1970
British Library Conference Proceedings | 2006
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