Flywheel simultaneous attitude control and energy storage using a VSCMG configuration

Space vehicle programs consistently endeavor to reduce satellite bus mass to increase payload capacity and/or reduce launch and fabrication costs. At the same time, performance demands on satellite systems continue to increase, creating a formidable challenge to space vehicle technology development....

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Bibliographic Details
Published in2000 IEEE International Conference on Control Applications pp. 991 - 995
Main Authors Fausz, J.L., Richie, D.J.
Format Conference Proceeding
LanguageEnglish
Published IEEE 2000
Subjects
Online AccessGet full text
ISBN9780780365629
0780365623
DOI10.1109/CCA.2000.897602

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