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- W2482495641 abstract "This paper considers the design of angular velocity observer for attitude control in small satellites under the presence of attitude measurement noise. Based on the contraction analysis, a set of exponentially convergent observers, namely, reduced-order, complete-order and synchronized observers is designed to deal with different level of the noise in the attitude measurements. Simulations are included to illustrate their performance." @default.
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- W2482495641 date "2016-03-01" @default.
- W2482495641 modified "2023-09-29" @default.
- W2482495641 title "Contraction based angular velocity observer for small satellites" @default.
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- W2482495641 doi "https://doi.org/10.1109/aero.2016.7500915" @default.
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