In this paper , the authors proposed an approach to adjust the attitude of a small satellite by using state-dependent coefficient parameterizations. But this approach is not suitable for large-scale systems
Spacecraft attitude reorientation with reaction wheel assembly via state-dependent coefficient parameterizations
Incremona, Gian Paolo;Yuca Huanca, Chrystian Pool Edmundo;Colaneri, Patrizio
2022-01-01
Abstract
In this paper , the authors proposed an approach to adjust the attitude of a small satellite by using state-dependent coefficient parameterizations. But this approach is not suitable for large-scale systemsFile in questo prodotto:
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