Observer-based Attitude Control In The Sliding Mode
Price
Free (open access)
Transaction
Volume
22
Pages
33
Published
1996
Size
2,636 kb
Paper DOI
10.2495/DCSS960411
Copyright
WIT Press
Author(s)
A.G. Luk'yanov, S.J. Dodds & J. Vittek
Abstract
With the increasing interest in small, relatively inexpensive satellites, envisaged to be produced on a large scale, there is a need to minimise development costs by embodying as many common elements as possible. The research presented here is aimed at the production of a 'universal' attitude controller in partial fulfilment of this need. Continuous momentum exchange torque actuators are assumed at present. Such a controller must maintain a specified dynamic response to changing
Keywords
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